nafd-061220-061
DESCRIPTION
nnnnTRANSCRIPT
TO 00-85-20TECHNICAL MANUAL
ENGINE SHIPPING INSTRUCTIONS(ATOS)
DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.
Published under authority of the Secretary of the Air Force
15 OCTOBER 2003 CHANGE 6 - 15 APRIL 2008
TO 00-85-20
INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.
LIST OF EFFECTIVE PAGESNOTE: The portion of the text affected by the changes is indicated by a vertical line in the outer
margins of the page. Changes to illustrations are indicated by shaded or screened areas,or by miniature pointing hands.
Dates of issue for original and changed pages are:
Original . . . . . . . . . . . . . . . . . . . . 0 . . . . . . . . . . 15 October 2003 Change . . . . . . . . . . . . . . . . . . . . 4 . . . . . . . . . . . . . . 15 June 2007Change . . . . . . . . . . . . . . . . . . . . 1 . . . . . . . . . . . . . . 30 July 2004 Change . . . . . . . . . . . . . . . . . . . . 5 . . . . . . . . . 1 December 2007Change . . . . . . . . . . . . . . . . . . . . 2 . . . . . . . . . . 27 October 2004 Change . . . . . . . . . . . . . . . . . . . . 6 . . . . . . . . . . . . . 15 April 2008Change . . . . . . . . . . . . . . . . . . . . 3 . . . . . . . . . . . . 15 March 2006
TOTAL NUMBER OF PAGES IN THIS MANUAL IS 122, CONSISTING OF THE FOLLOWING:
Page *Change Page *Change Page *ChangeNo. No. No. No. No. No.
Title . . . . . . . . . . . . . . . . . . . . . . . . . 6A . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6i - iv . . . . . . . . . . . . . . . . . . . . . . . . . 11-1 . . . . . . . . . . . . . . . . . . . . . . . . . . . 51-2 - 1-4 . . . . . . . . . . . . . . . . . . . . . 02-1 . . . . . . . . . . . . . . . . . . . . . . . . . . . 42-2 Blank . . . . . . . . . . . . . . . . . . . . 03-1 - 3-12 . . . . . . . . . . . . . . . . . . . . 04-1 . . . . . . . . . . . . . . . . . . . . . . . . . . . 44-2 - 4-3 . . . . . . . . . . . . . . . . . . . . . 04-4 . . . . . . . . . . . . . . . . . . . . . . . . . . . 44-4.1 . . . . . . . . . . . . . . . . . . . . . . . . . 44-4.2 Blank . . . . . . . . . . . . . . . . . . . 34-5 - 4-11 . . . . . . . . . . . . . . . . . . . . 04-12 . . . . . . . . . . . . . . . . . . . . . . . . . 34-13 . . . . . . . . . . . . . . . . . . . . . . . . . 04-14 . . . . . . . . . . . . . . . . . . . . . . . . . 64-15 - 4-19 . . . . . . . . . . . . . . . . . . . 04-20 Blank . . . . . . . . . . . . . . . . . . . 05-1 - 5-9 . . . . . . . . . . . . . . . . . . . . . 05-10 Blank . . . . . . . . . . . . . . . . . . . 05-11 . . . . . . . . . . . . . . . . . . . . . . . . . 05-12 Blank . . . . . . . . . . . . . . . . . . . 05-13 . . . . . . . . . . . . . . . . . . . . . . . . . 05-14 Blank . . . . . . . . . . . . . . . . . . . 05-15 - 5-17 . . . . . . . . . . . . . . . . . . . 05-18 Blank . . . . . . . . . . . . . . . . . . . 06-1 . . . . . . . . . . . . . . . . . . . . . . . . . . . 46-2 - 6-27 . . . . . . . . . . . . . . . . . . . . 06-28 - 6-31 . . . . . . . . . . . . . . . . . . . 26-32 - 6-33 . . . . . . . . . . . . . . . . . . . 06-34 . . . . . . . . . . . . . . . . . . . . . . . . . 26-35 . . . . . . . . . . . . . . . . . . . . . . . . . 06-36 . . . . . . . . . . . . . . . . . . . . . . . . . 66-37 - 6-52 . . . . . . . . . . . . . . . . . . . 07-1 - 7-6 Added . . . . . . . . . . . . . . . 1
*Zero in this column indicates an original page
A Change 6 USAF
T.O. 00-85-20
TABLE OF CONTENTS
Chapter Page
1 INTRODUCTION ...........................................................................................................................................................1-1
1.1 Purpose...............................................................................................................................................................1-11.3 Application.........................................................................................................................................................1-11.4 Pertinent Directives ...........................................................................................................................................1-11.5 Movement Planning Guide................................................................................................................................1-11.6 Surface Transit Guide........................................................................................................................................1-2
2 RESPONSIBILITIES.......................................................................................................................................................2-1
2.1 Shipping and Receiving Activities....................................................................................................................2-12.2 Recommended Technical Order Changes ........................................................................................................2-1
3 ENGINE SHIPPING DEVICES .....................................................................................................................................3-1
3.1 General Information ..........................................................................................................................................3-13.2 Shipment Center of Gravity (Center of Balance) ............................................................................................3-1
4 PREPARATION AND INSPECTION ...........................................................................................................................4-1
4.1 General Information ..........................................................................................................................................4-14.2 Required Documents and Entries......................................................................................................................4-14.3 Preparation for Shipment ..................................................................................................................................4-24.4 Shipments on Transportation Trailers, Skids or Dollies ..................................................................................4-24.5 Shipments in Engine Containers (Steel, Reusable) ..........................................................................................4-44.6 Shipments in Engine Module Containers (Steel and Fiberglass Reinforced Plastic (FRP), Reus-
able)...............................................................................................................................................................4-74.7 Shipments in Wood Boxes................................................................................................................................4-74.8 Shipping of Engines with Installed Afterburners ...........................................................................................4-124.9 Inspections .......................................................................................................................................................4-124.10 Engine Records................................................................................................................................................4-134.11 Shipment of J79 Engines with Afterburner and Quick Engine Change (QEC) Kit Installed on
Trailer..........................................................................................................................................................4-134.12 F101-GE-102 Engine Deviations to Shipping Instructions............................................................................4-134.13 F118-GE-100 Engine Deviations to Shipping Instructions............................................................................4-144.14 F118-GE-101 Engine Deviations to Shipping Instructions............................................................................4-14
5 ENGINE AND SHIPPING DEVICE HANDLING .......................................................................................................5-1
5.1 Equipment ..........................................................................................................................................................5-15.3 Handling Engines in Metal and FRP Containers by Forklift ..........................................................................5-15.10 Handling Engines on Dollies or Trailers..........................................................................................................5-25.14 Loading F108/Multi-Purpose Trailer onto Flatbed with Forklift Figure 5-1, Figure 5-2 and table
4-3) ................................................................................................................................................................5-25.15 Loading F108/Stand (Part Number 856A1200) onto Flatbed with Figure 6-14, Figure 6-15 and
table 4-3) .......................................................................................................................................................5-45.16 Transportation of Jet Engines by Towing ........................................................................................................5-55.17 Additional Towing Instructions for F108 Engine/Multi-Purpose Trailer (ETU-111/E) .................................5-65.18 Compact Aircraft Support Package ..................................................................................................................5-6
6 TIE DOWN INSTRUCTIONS .......................................................................................................................................6-1
6.1 General...............................................................................................................................................................6-16.6 Rail Shipment ....................................................................................................................................................6-1
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6.7 Airlift Shipment.................................................................................................................................................6-16.8 Truck Shipment .................................................................................................................................................6-26.9 Certification and Seals ......................................................................................................................................6-36.10 Loading United Trailer for Air Transport ......................................................................................................6-116.11 Loading Lockheed Engine Trailer in Aircraft, TF39.....................................................................................6-126.12 Loading Engine Trailer on Flat Bed Truck or Railway Flat Car, TF39.......................................................6-126.13 Tiedown Instructions for Multi-Purpose Trailer, F108..................................................................................6-146.14 Tiedown Instructions for F108 Engine Stand (Part Number 856 Figure 6-16)............................................6-146.15 F110 Engine Shipping and Storage Stand General Information ...................................................................6-156.16 ETU-114/E Stand Surface Transportation, F110 ...........................................................................................6-156.17 Placement for the Shipment of 1, 2, 3 and 4 Engines, F110 ........................................................................6-166.17.1 One engine:......................................................................................................................................................6-166.17.2 Two engines:....................................................................................................................................................6-166.17.3 Three engines:..................................................................................................................................................6-166.17.4 Four engines: ...................................................................................................................................................6-166.18 Air Transportation, F110 (Figure 6-20)..........................................................................................................6-206.19 Unstacking ETU-114/E Stand, F110 ..............................................................................................................6-206.20 Loading TT90-F-503/TT90-F-505 Trailer and F117-PW-100 on a Flat Bed Trailer Using Tow
Vehicle ........................................................................................................................................................6-286.21 Loading TT90-F Trailer in Aircraft, F117-PW-100.......................................................................................6-296.22 Loading 150504-1 Instructions for Surface Transportation, F117-PW-100..................................................6-346.23 F118-GE-101 Engine Tie Down Instructions for Trailer (Part Number 75GH109).....................................6-366.24 Loading and Transportation for F119 Engine ................................................................................................6-396.25 Purpose.............................................................................................................................................................6-396.26 General Information ........................................................................................................................................6-396.27 Inspection of 3000E Transportation Trailer ...................................................................................................6-396.28 Positioning of F119/ESS On 3000E Transportation Trailer..........................................................................6-396.29 F119 Engine Shipping Instructions.................................................................................................................6-396.29.1 F119 Engine Ground Transport Shipping Instructions ..................................................................................6-406.29.2 Loading F119/ESS/3000E Engine On Ground Transport Vehicle................................................................6-406.29.3 Roll On Loading (Preferred Method) .............................................................................................................6-406.29.4 Lift On Loading (Permitted Only If Loading Ramp Is Unavailable) ...........................................................6-406.29.5 Hoist On Loading Is Not Permitted ...............................................................................................................6-416.29.6 F119 Engine Air Transport Shipping Instructions (For ESS/3000E Trailer Mounted Engines
Only) ...........................................................................................................................................................6-416.29.7 Loading F119 Engine on Transport Aircraft..................................................................................................6-426.29.8 Roll On Loading (Only Approved Method) ..................................................................................................6-426.29.9 Lift On Loading Is Not Permitted ..................................................................................................................6-426.29.10 Hoist On Loading Is Not Permitted ...............................................................................................................6-426.29.11 Securing F119 Engine in Transport Aircraft..................................................................................................6-42
7 ENGINE SHIPPING DEVICE MANAGEMENT..........................................................................................................7-1
LIST OF ILLUSTRATIONS
Number Title Page
1-1 Mileage Chart ...........................................................................................................................................................1-31-2 Aircraft Dimensions..................................................................................................................................................1-43-1 Vehicle Center of Gravity Formula .........................................................................................................................3-14-1 Engine in a Flexible Environmental Container .......................................................................................................4-64-2 Tie Down Diagram for Airlift Trailers Transported on Trucks .............................................................................4-84-3 Pneumatic Suspension (Air Ride) Truck and Trailer (Typical)............................................................................4-104-4 Tie Down Diagram for Air Lift of Trailer ............................................................................................................4-154-5 Two Engine Tie Down...........................................................................................................................................4-164-6 One Engine Tie Down ...........................................................................................................................................4-17
ii Change 1
T.O. 00-85-20
4-7 Two Engine Tie Down...........................................................................................................................................4-184-8 One Engine Tie Down ...........................................................................................................................................4-195-1 Multi-Purpose Trailer - F-108 Engine .....................................................................................................................5-85-2 Hydraulic System......................................................................................................................................................5-95-3 APU/Eng Change Support......................................................................................................................................5-115-4 Tool Box Support ...................................................................................................................................................5-135-5 Rails ........................................................................................................................................................................5-155-6 Tire Rack ................................................................................................................................................................5-165-7 Rail Modification....................................................................................................................................................5-176-1 Side View of Trailer Mounted Engine Loaded for Open Truck Shipment ...........................................................6-36-2 Front View of Trailer Mounted Engine Loaded for Open Truck Shipment..........................................................6-46-3 Close-Up View of Tie Down at Engine Mount ......................................................................................................6-46-4 Trailer 55J9109 with KC-97 Power Package Installed, Right Rear
Three-Quarter View............................................................................................................................................6-56-5 Trailer 55J9109 with KC-97 Power Package Installed, Left Front
Three-Quarter View............................................................................................................................................6-56-6 Recommended Tiedown Position for Air Shipment ...............................................................................................6-66-7 Engine Containers Double Decked ..........................................................................................................................6-76-8 Engine Tie Down for Flat Car on Truck Shipment ................................................................................................6-76-9 Shipment of Engine Transportation Trailers ...........................................................................................................6-96-10 Shipment of Engine Transportation/Installation Trailers ......................................................................................6-106-11 Position of Tiedown Chains or Cables ..................................................................................................................6-136-12 Front Tiedown ........................................................................................................................................................6-176-13 Rear Tiedown..........................................................................................................................................................6-186-14 Side Tiedowns (2 sides) .........................................................................................................................................6-196-15 Surface Transportation, F110 .................................................................................................................................6-216-16 F108 Transportation Stand Tie Down ...................................................................................................................6-226-17 F108 Transportation Stand Tie-Down (Alternate Method)...................................................................................6-236-18 Nylon Strap Tiedown (Preferred Method).............................................................................................................6-246-19 Chain Tiedown (Alternate Method) .......................................................................................................................6-256-20 Stack Stand Tiedown..............................................................................................................................................6-266-21 HCU-6/E Pallet Tiedown .......................................................................................................................................6-276-22 Transportation Trailer Tiedown Configuration (Flatbed Truck)...........................................................................6-306-23 Transportation Trailer Tiedown Configuration......................................................................................................6-326-24 Truck Trailer Tie-Down .........................................................................................................................................6-356-25 F118-GE-101 Engine Tie Down Procedure...........................................................................................................6-386-26 F119/ESS/3000E Overall Dimensions and Truck Tiedown Configuration - Front View ...................................6-436-27 F119/ESS/3000E Overall Dimensions and Truck Tiedown Configuration - Side View.....................................6-446-28 F119/ESS/3000E Overall Dimensions and Truck Tiedown Configuration - Plan View.....................................6-456-29 Positioning of Heavy Duty Forklift Tines for Lifting F119/ESS/3000E onto a Flatbed Truck..........................6-466-30 Tighten Rail Clamps to 375-400 IN LBF .............................................................................................................6-476-31 Block and Secure Towbar to Truckbed .................................................................................................................6-486-32 Block and Chock 3000E Trailer Tires On Truck Bed..........................................................................................6-496-33 F119/ESS/3000E Overall Dimensions and Cargo Aircraft Tiedown Configuration - Front View.....................6-506-34 F119/ESS/3000E Overall Dimensions and Cargo Aircraft Tiedown Configuration - Side View ......................6-516-35 F119/ESS/3000E Overall Dimensions and Cargo Aircraft Tiedown Configuration - Plan View ......................6-52
LIST OF TABLES
Number Title Page
3-1 Trailers.........................................................................................................................................................................3-23-2 Adapters.....................................................................................................................................................................3-113-3 Shipping Device Weights .........................................................................................................................................3-124-1 Container Temperature vs. Nitrogen Pressure ...........................................................................................................4-54-2 Recommended Torque Values for Container, Trailer and Adapter Bolts ................................................................4-96-1 Trailer ........................................................................................................................................................................6-36
Change 1 iii
T.O. 00-85-20
6-2 Trailer ........................................................................................................................................................................6-366-3 Shipping Device Weights .........................................................................................................................................6-367-1 Engine Shipping Devices - First Column Identifier Codes.......................................................................................7-27-2 Engine Shipping Devices - Trailers - Second and Third Column Identifier Codes.................................................7-27-3 Engine Shipping Devices - Adapters - Fourth Column Identifier Codes .................................................................7-37-4 Engine Shipping Devices - Containers - Second, Third and Fourth Position Codes...............................................7-4
iv Change 1
TO 00-85-20
CHAPTER 1INTRODUCTION
1.1 PURPOSE.
1.2 This technical order provides information and instructions for handling and shipping of Air Force engines. Because ofthe variations in engines and shipping devices some of the information in this manual is general in nature. When generalinstructions are given, the intent shall be fulfilled. Lack of specific details shall not constitute authority or permission todeviate from the intent of any instructions. Total compliance with these instructions shall be mandatory upon activities whichhave physical custody of the engine. The procedures outlined here are based on actual practices which have proved to be bothpractical and necessary in the protection of propulsion systems.
1.3 APPLICATION.
1.3.1 This technical order applies to all Air Force activities and contractors shipping Air Force engines. Only those deviceslisted in section III are authorized for shipment of engines without express written permission of the Engine InventoryManagement at the responsible ALC.
1.3.2 Airlift trailers, stands and dollies shall be used for air shipment of engines when available. When not available, or ascircumstances require, metal or FRP containers may be used. Shipments of metal containers will be allowed afterpreservation of the fuel system and the container is pressurized in accordance with engine handbooks, TO 2J-1-18 or TO 2R-1-11.
1.4 PERTINENT DIRECTIVES.
The following directives are important for the proper shipping of Air Force engines.
TO 2J-1-18 Corrosion Control of Jet Engines
TO 2R-1-11 Corrosion Control of Reciprocating Engines
AFMAN 24-204(I) Packaging and Handling of Dangerous Materials for Transportation by Military Aircraft
AFI 24-201 Function and Responsibilities of Transportation Activities
AFJI 24-228 Reporting of Transportation Discrepancies in Shipment
Military standards are referenced throughout this technical order.
1.5 MOVEMENT PLANNING GUIDE.
NOTE
The Transportation Officer should notify trucking companies when ordering trailers that only wood beds areacceptable as the Air Force has no available means of tying down to metal beds, trailers, or trucks.
1.5.1 Many facets must be considered in the selection of the mode of transportation to be used. Some of these are: weather,availability of preferred mode and carrier, distance, required delivery date (RDD), etc. Each shipment will have its ownpeculiarities, e.g., type of package, dimensions, freight, etc. Shipping activities must therefore plan and manage each andevery shipment on its individual requirements. The standard transit time for aircraft jet engines moving within the CONUS isfour (4) days. One exception is the required delivery date as reflected in RDD block of shipping document (DD Form 1348-1), and is a factor to be considered in determining mode selection. This capability provides transportation an area of selectionbetween shipping a specific engine on either an expedited or routine basis and at the same time effect delivery service tosatisfy requirements of user or Specialized Repair Activity (SRA). It behooves each and every traffic manager to select amode and carrier that can and does meet or exceed this criteria. Use of two drivers in conjunction with “exclusive use of
Change 5 1-1
TO 00-85-20
vehicle” is authorized when an RDD dictates same. The pertinent Military Traffic Management Command (MTMC) agencymust be informed of these requirements and decisions. You will challenge MTMC if their routings do not satisfy yourrequirements and in cases where carrier availability is a problem, alternate carriers should be requested.
1.6 SURFACE TRANSIT GUIDE.
1.6.1 The following transit times are based on an average. Weather, adverse road conditions, and highway traffic congestionare taken into consideration.
1.6.1.1 Class “A” Carriers.
1.6.1.1.1 Less than truck load (LTL) - Calculate approximately 300 miles per day maximum. This will be reduced whenroutes transit metropolitan areas and gateway terminals.
1.6.1.1.2 Truck load (TL) - Will normally insure expedited movement from carrier’s terminal but not necessarily reducedoverall transit time unless exclusive use of vehicle is requested. This enables a serialized seal to be affixed and prevents delayat gateway points, but does not guarantee more than 500 miles transit daily.
1.6.1.2 Heavy Haulers Specialized Carriers.
1.6.1.2.1 Less than truck load (LTL) - This mode, with exceptions, can be beneficial from both a monetary and transit timeviewpoint. Often a particular carrier will be “dead heading” equipment from point “A” to point “B” and an engine can bedestined to a point enroute or at the terminus. Bills of lading shall be annotated “TENDERED AS AN LTL” to insure propercharges are affixed by the carrier.
1.6.1.2.2 Truck (TL) - This mode normally affords the most expeditious surface transportation. Two drivers with sleeperaccommodations will normally insure eight to nine hundred miles transit each twenty-four hours.
1.6.1.2.3 Expedited service obviously is more costly than normal LTL rates. Each movement must therefore be consideredon its own merits. The minimum cost mode should be selected that will deliver aircraft engines to the consignee by deliverydate or UMMIPS. Note mileage chart (Figure 1-1).
1-2
TO 00-85-20
Figure 1-1. Mileage Chart
1-3
TO 00-85-20
*DOOR DIMENSIONS *CABIN DIMENSIONSTYPE
AIRCRAFT WIDE HIGH LONG WIDE HIGHC54 65” X 93” 595 X 92 X 102
C97 171” X 91” 762 X 102 X 96
C118 123” X 75” 816 X 104 X 93
C121 104” X 74” 984 X 120 X 84
C123 109” X 75” 444 X 109 X 75
C124 135” X 138” 882 X 135 X 138
C130 123” X 109” 492 X 122 X 109
C135 115” X 78” 858 X 127 X 84
**C141 123″ X 109″ 840 X 122 X 109
CL-44 136” X 80” 1008 X 136 X 80
C-5A FWD X 161” 1453 X 228 X 161228”
C-5A AFT X 134” 1453 X 228 X 161228”
DC7 78” X 124” 816 X 93 X 104
DC9 136” X 81” 822 X 114 X 81
L188 140” X 80” 825 X 78 X 87
L100 123” X 109” 584 X 120 X 111
C-17A 216” X 177” 1016 X 216 X 158
NOTE
This chart can be used as a guide to determine the type engine that can be loaded on various types of cargoaircraft. Dimensions will vary slightly within “TYPE OF AIRCRAFT” due to model.
*Door and Cabin dimensions are reduced in height by four inches on all aircraft equipped with the 463L system.
**This height reduced to 106″ by AFT pressure door latches when truck bed loading.
Figure 1-2. Aircraft Dimensions
1-4
TO 00-85-20
CHAPTER 2RESPONSIBILITIES
2.1 SHIPPING AND RECEIVING ACTIVITIES.
Responsibility for compliance with the technical order rests with the shipping and receiving activities in accordance withDepartment of Transportation regulations and AFMAN 24-201.
NOTE
The Transportation Officer should notify trucking companies when ordering trailers that only wood beds areacceptable as the Air Force has no available means of tying down to metal beds, trailers, or trucks.
2.1.1 The transportation officer of the shipping activity has the authority and responsibility to inspect and reject any vehiclewhich is considered unsatisfactory for engine shipment. This responsibility includes condition of transporting vehicle, properloading, blocking, bracing, and documenting to prevent engine damage and assure expeditious delivery to ultimate consignee.
2.1.2 The transportation officer will reject any engine which has not been properly prepared for shipment in accordancewith AFMAN 24-204, TO 2J-1-18, TO 2R-1-11, or NAVAIR 15-02-500.
2.1.3 Shipments reviewed intransit or terminating shall be visually inspected at each ON/OFF loading terminal for damageor unsatisfactory condition. Any damage or unsatisfactory conditions noted will be reported in accordance with AFMAN 24-201, Transportation Cargo Movement, or AFR 75-18.
2.1.4 In the event a trailer mounted engine is found leaking during air transit the engine will be removed from the aircraft atnext destination and properly prepared in accordance with TO 2J-1-18. The engine will then be placed back into thetransportation cycle for completion of shipment to primary destination.
NOTE
A DD FORM 6 will be prepared in accordance with AFI 24-201.
2.1.5 Shipments reviewed in transit or terminating shall be visually inspected at each ON/OFF loading terminal for damageor unsatisfactory condition. Any damage or unsatisfactory conditions noted will be reported in accordance with AFI 24-201or AFR 75-18. Engines being received at terminating points, which are covered by plastic cover, will be inspected fordamage prior to off loading from carriers equipment. To insure a thorough inspection is accomplished, removal of plasticcover is required, also for photographs if damage is detected. Damage detected should be noted on carrier’s deliverydocument while facts are current and available.
2.1.6 Upon completion of inspection, engine will be rewrapped to comply with instructions contained in Chapter 4,paragraph 4.1.2 .
2.2 RECOMMENDED TECHNICAL ORDER CHANGES.
Recommendations for amendments to this technical order should be forwarded to Oklahoma City ALC/LPARP on AFTOFORM 22, TECHNICAL ORDER SYSTEM PUBLICATION IMPROVEMENT REPORT AND REPLY, in accordancewith TO 00-5-1. To maintain this technical order current and adequate it shall be the responsibility of the prime shippingdevice item manager to review and update it as follows:
2.2.1 Addition of new equipment.
2.2.2 Changes in national stock number, part number, dimensions or special instructions concerning equipment.
2.2.3 Deletion of obsolete or discontinued equipment.
Change 4 2-1/(2-2 blank)
TO 00-85-20
CHAPTER 3ENGINE SHIPPING DEVICES
3.1 GENERAL INFORMATION.
This section lists the different types of shipping devices. Each engine has been listed along with its appropriate shippingdevice, national stock number (NSN) and part number (PN). Dimensions, weights, and shipping codes have also been listedwhere appropriate. Gross weights include engine, shipping device, adapters, plugs, required desiccant and preservation whenused. Dimensions are stated to the nearest full inch. The weights indicated herein are average for the item named and it ispossible that some variance will be noted. Therefore, all engines tendered for air shipment should be weighed before beingreleased. Report significant differences in accordance with Table 3-1, page 3-2.
3.2 SHIPMENT CENTER OF GRAVITY (CENTER OF BALANCE).
3.2.1 Marking of center of gravity (center of balance) will be in accordance with MIL-STD-129.
3.2.2 The center of gravity (center of balance) of a loaded wooden, FRP, or metal engine container is that location along thelength of the container at which the container will balance on a fulcrum placed under and at right angels to the length of thecontainer. The container may be placed on a single cross roller and moved until a balance point is reached.
3.2.3 The following formula shall be used for determining the center of gravity (center of balance) for aircraft enginesmounted on trailers being shipped via aircraft.
3.2.3.1 Weight loaded trailer.
3.2.3.2 Weight both rear wheels.
3.2.3.3 Measure wheel base hub to hub.
3.2.3.4 Use formula per Figure 3-1.
VEHICLE C.G. FORMULA:
A. REAR AXLE WEIGHT x WHEEL BASE = VEHICLE C.G. IN INCHES AFT OF FRONT AXLEVEHICLE GROSS WEIGHT
Figure 3-1. Vehicle Center of Gravity Formula
3-1
TO 00-85-20
3-2
Tab
le 3
-1.
Tra
ilers
Nat
ion
alD
imen
sio
ns
Sto
ckP
art
(Les
s D
raw
En
gin
eD
evic
eG
ross
Sh
ipp
ing
En
gin
eN
um
ber
Nu
mb
erB
ar)
Wei
gh
tW
eig
ht
Wei
gh
tC
od
e*a.
Des
crip
tion.
Car
go t
o be
tra
nspo
rted
is
basi
cally
com
pris
ed o
f ai
rcra
ft e
ngin
es a
nd t
heir
shi
ppin
g de
vice
s lis
ted
belo
w.
b. C
onfi
gura
tion.
App
roxi
mat
e ch
arac
teri
stic
s of
Okl
ahom
a C
ity A
LC
pri
me
engi
nes
mos
t fr
eque
ntly
shi
pped
:
F101
-GE
-102
1740
-00-
713-
1076
4018
5.5x
58 1
/2x9
948
2474
055
64SA
5908
1740
-00-
580-
1057
2214
0x73
x74
4135
980
5115
SA04
94
F108
1740
-01-
127-
STC
9085
6-1
170x
67x9
746
7232
0078
72SA
4954
F110
-GE
-100
1740
-00-
713-
1076
4018
.5x5
8.5x
9938
6574
047
05SA
5908
F110
-GE
-129
1740
-00-
713-
1076
4018
.5x5
8.5x
9939
8074
047
80SA
5908
F117
PW-1
0017
40-0
1-45
7-T
T90
-F-5
0332
2x96
x60
1150
027
0025
200
SA99
75
J-57
-19W
1740
-00-
516-
1003
1515
6x59
x74
3970
690
4660
SA79
30
1740
-00-
713-
5908
1740
-00-
554-
1046
2415
7x73
x74
3970
930
4900
SA16
67
1740
-00-
580-
1057
2215
6x73
x74
3970
860
4830
SA04
94
J-57
-21
2317
40-0
0-51
6-10
0315
168x
59x7
446
1569
053
05SA
7930
1740
-00-
713-
1076
4016
8x59
x74
4615
840
5455
SA59
08
1740
-00-
554-
1046
2416
8x73
x74
4615
930
5545
SA16
67
1740
-00-
580-
1057
2216
8x73
x74
4615
860
5475
SA04
94
J-57
-29
1740
-00-
516-
7930
1740
-00-
713-
1076
4015
6x59
x74
3820
840
4660
SA59
08
TO 00-85-20
3-3
Tab
le 3
-1.
Tra
ilers
- C
onti
nued
Nat
ion
alD
imen
sio
ns
Sto
ckP
art
(Les
s D
raw
En
gin
eD
evic
eG
ross
Sh
ipp
ing
En
gin
eN
um
ber
Nu
mb
erB
ar)
Wei
gh
tW
eig
ht
Wei
gh
tC
od
e*17
40-0
0-55
4-10
4624
156x
73x7
438
2093
047
50SA
1667
1740
-00-
580-
1057
2215
6x73
x74
3820
860
4680
SA04
94
J-57
-43W
B17
40-0
0-51
6-10
0315
156x
59x7
437
7069
044
60SA
7930
1740
-00-
713-
1076
4015
6x59
x74
3770
840
4610
SA59
08
1740
-00-
554-
1046
2415
6x73
x74
3770
930
4700
SA16
67
1740
-00-
580-
1057
2215
6x73
x74
3770
860
4630
SA04
94
J-57
-55
1740
-00-
516-
1003
1515
6x59
x74
5259
690
5949
SA79
30
1740
-00-
713-
1076
4015
6x59
x74
5259
840
6099
SA59
08
1740
-00-
554-
1046
2415
6x73
x74
5259
930
6189
SA16
67
1740
-00-
580-
1057
2215
6x73
x74
5259
860
6119
SA04
94
J-57
-59
1740
-00-
516-
1003
1515
6x59
x74
4364
690
5054
SA79
30
1740
-00-
713-
1076
4015
6x59
x74
4364
840
5204
SA59
08
1740
-00-
554-
1046
2415
6x73
x74
4364
930
5294
SA16
67
1740
-00-
580-
1057
2215
6x73
x74
4364
860
5224
SA04
94
J-57
1740
-00-
713-
1076
4015
2x59
x74
5155
825
5980
SA59
08
J-79
1740
-00-
713-
1076
4013
2x59
x74
3150
880
4030
SA59
08
1740
-00-
516-
1003
1513
2x59
x74
3150
730
3880
SA79
30
TO 00-85-20
3-4
Tab
le 3
-1.
Tra
ilers
- C
onti
nued
Nat
ion
alD
imen
sio
ns
Sto
ckP
art
(Les
s D
raw
En
gin
eD
evic
eG
ross
Sh
ipp
ing
En
gin
eN
um
ber
Nu
mb
erB
ar)
Wei
gh
tW
eig
ht
Wei
gh
tC
od
e*17
40-0
0-55
4-10
4624
132x
73x7
431
5097
041
20SA
1667
1740
-00-
580-
1057
4413
2x73
x74
3150
900
4050
SA04
94
TF3
017
40-0
0-58
0-10
5722
140x
73x7
441
3598
051
15SA
0494
1740
-00-
554-
1046
2414
0x73
x74
4135
1050
5185
SA16
67
1740
-00-
516-
1003
1514
0x59
x74
4135
810
4945
SA79
30
1740
-00-
713-
1076
4014
0x59
x74
4135
960
5095
SA59
08
TF3
3-17
40-0
0-55
4-10
4624
140x
73x8
543
0011
5054
50SA
P3/P
5/P9
/P10
3/16
67P1
02/P
105
1740
-00-
580-
1057
2214
0x73
x85
4300
1080
5380
SA04
94
TF3
3-P7
P10
017
40-0
0-55
4-10
4624
140x
73x8
547
5011
5059
00SA
1667
1740
-00-
580-
1057
2214
0x73
x85
4750
1080
5830
SA04
94
TF4
117
40-0
0-51
6-10
0315
132x
59x8
231
9097
041
60SA
7930
1740
-00-
713-
1076
4013
2x59
x82
3190
1120
4310
SA59
08
T58
-3/5
1740
-00-
690-
1032
3832
x44x
6133
545
078
5SA
5284
T65
-7-7
A17
40-0
0-71
3-10
7640
132x
44x6
171
275
014
62SA
5908
c. C
onfi
gura
tion.
App
roxi
mat
e ch
arac
teri
stic
s of
San
Ant
onio
AL
C p
rim
e en
gine
s m
ost
freq
uent
ly s
hipp
ed:
F100
-PW
-220
1076
4021
5x59
x87
3085
1479
4564
SA
F100
-100
1740
-00-
713-
1076
4021
5x59
x87
3085
1479
4564
SA59
08
F100
-200
1740
-00-
713-
1076
4021
5x59
x87
3085
1479
4564
SA59
08
TO 00-85-20
3-5
Tab
le 3
-1.
Tra
ilers
- C
onti
nued
Nat
ion
alD
imen
sio
ns
Sto
ckP
art
(Les
s D
raw
En
gin
eD
evic
eG
ross
Sh
ipp
ing
En
gin
eN
um
ber
Nu
mb
erB
ar)
Wei
gh
tW
eig
ht
Wei
gh
tC
od
e*T
5617
40-0
0-71
3-10
7640
132x
59x7
413
2690
022
26SA
5908
1740
-00-
516-
1003
1513
2x59
x74
1326
750
2076
SA79
30
T56
1740
-00-
718-
4041
90-1
1326
750
2076
SA15
79
-313
2675
020
76SA
J60
1740
-00-
690-
1072
3813
2x44
x61
460
450
910
SA52
84
J65
1740
-00-
516-
1003
3413
2x59
x40
2690
500
3190
SA79
29
TF3
417
40-0
0-55
4-30
1013
2x35
x73
1443
1480
2923
SA16
67
TF3
417
40-0
0-71
3-30
00A
152x
40x5
8 1/
214
4315
1029
53SA
5908
F100
1740
-00-
516-
1003
1521
2x59
x87
3085
1329
4414
SA79
30
1740
-00-
554-
1046
2421
2x73
x87
3085
1569
4654
SA16
67
1740
-00-
580-
1057
2221
2x73
x87
3085
1499
4584
SA04
94
1740
-00-
713-
1076
4021
2x59
x87
3085
1479
4564
SA59
08
1730
-01-
038-
ET
U-1
00/E
73-x
48x5
830
8565
037
35SA
1371
F100
-100
1740
-00-
713-
1076
4021
2x59
x87
3085
1479
4564
SA59
08
F100
-200
1740
-00-
713-
1076
4021
2x59
x87
3085
1479
4564
SA54
08
F110
-GE
-100
1730
-NC
D-
ET
U-1
14/E
90x4
8x56
3965
1020
4985
SA17
7309
F110
-GE
-129
1730
-NC
D-
ET
U-1
14/E
90x4
8x56
3980
1020
5010
SA17
7309
TF3
917
40-0
0-48
8-U
A53
3560
-230
1x11
1x11
572
6012
040
1930
0SA
9469
TO 00-85-20
3-6
Tab
le 3
-1.
Tra
ilers
- C
onti
nued
Nat
ion
alD
imen
sio
ns
Sto
ckP
art
(Les
s D
raw
En
gin
eD
evic
eG
ross
Sh
ipp
ing
En
gin
eN
um
ber
Nu
mb
erB
ar)
Wei
gh
tW
eig
ht
Wei
gh
tC
od
e*17
40-0
0-60
2-4S
3003
1-10
1A25
5x11
0x11
472
6091
8016
440
SA63
65
T70
017
40-0
0-43
5-22
142
7818
*SH
IPPI
NG
CO
DE
A.
Suita
ble
for
air
ship
men
t or
on-
base
mov
emen
t on
ly.
S. S
uita
ble
for
surf
ace
ship
men
t or
on-
base
mov
emen
t on
ly.
SA.
Suita
ble
for
surf
ace
or a
ir s
hipm
ent
or o
n-ba
se m
ovem
ent.
Tra
iler
Inte
rcha
ngea
bilit
y:
F100
Eng
ines
: -1
00 -
200
1740
-00-
713-
5908
- 1
740-
00-5
16-7
930
All
J57
Eng
ines
:17
40-0
0-51
6-79
30 -
174
0-00
-713
-590
8
All
TF3
0-T
F33
Eng
ines
:17
40-0
0-55
4-16
67 -
174
0-00
-580
-049
4
All
TF4
1-T
F41A
1 E
ngin
es:
1740
-00-
516-
7930
- 1
740-
00-7
13-5
908
All
J75:
Onl
y 17
40-0
0-71
3-59
08
All
T70
0:17
30-0
0-43
5-78
18
F107
-WR
-101
8145
-01-
125-
1121
4-53
10-1
35.2
5x27
.0x5
7.0
156
140
296
1478
AN
F107
-WR
-400
8145
-01-
125-
1121
4-53
10-2
35.2
5x27
.0x5
7.0
148
142
290
1473
AN
F112
-WR
-100
8145
-01-
206-
1121
4-67
92-1
31.5
x31.
0x43
.027
613
441
098
89A
N
J35-
3581
45-0
0-39
0-60
012
5x66
x70
1782
2090
3872
5568
J47-
2581
45-0
0-30
8-50
8E66
713
8x53
x58
2365
1775
4140
4814
J47-
2781
45-0
0-30
8-50
8E66
713
8x53
x58
2475
1775
4250
4814
J52-
381
45-0
0-68
0-P1
3721
194x
62x7
421
8938
0059
8923
21
J57-
1381
45-0
0-58
7-P1
2888
194x
62x7
350
6938
0088
6924
31
J57-
1981
45-0
0-58
7-P1
2888
194x
62x7
339
7038
0077
7024
31
TO 00-85-20
3-7
Tab
le 3
-1.
Tra
ilers
- C
onti
nued
Nat
ion
alD
imen
sio
ns
Sto
ckP
art
(Les
s D
raw
En
gin
eD
evic
eG
ross
Sh
ipp
ing
En
gin
eN
um
ber
Nu
mb
erB
ar)
Wei
gh
tW
eig
ht
Wei
gh
tC
od
e*J5
7-21
8145
-00-
587-
P128
8819
4x62
x73
4615
3800
8415
2431
J57-
2381
45-0
0-58
7-P1
2888
194x
62x7
346
1538
0084
1524
31
J57-
2981
45-0
0-58
7-P1
2888
194x
62x7
338
2038
0076
2024
31
J57-
4381
45-0
0-58
7-P1
2888
194x
62x7
337
7038
0075
7024
31
J57-
5381
45-0
0-58
7-P1
2888
194x
62x7
350
8938
0088
8924
31
J57-
5581
45-0
0-58
7-P1
2888
194x
62x7
352
5938
0090
5924
31
J57-
59W
8145
-00-
587-
P128
8819
4x62
x73
4320
3800
8120
2431
J57-
5981
45-0
0-58
7-P1
2888
194x
62x7
343
6438
0081
6424
31
J60
AL
L81
45-0
0-84
5-P2
4984
96x4
8x54
460
905
1365
7668
J65
AL
L81
45-0
0-39
0-41
9194
133x
59x6
526
9021
0047
9055
74
J69-
2581
45-0
0-29
2-56
5081
-174
x40x
4338
068
610
6696
42
J71-
11,
A13
8145
-00-
597-
6800
032
200x
64x7
540
0027
2567
2557
72
8145
-00-
598-
6738
6223
2x64
x75
4000
5150
9150
7848
T70
081
45-0
1-05
9-81
45C
ON
004-
156
89A
N
T70
0-G
E-7
0081
45-0
0-77
2-25
x47
423
7870
Eng
ine
Nat
iona
lPa
rtD
imen
sion
Eng
ine
Dev
ice
Gro
ssSh
ippi
ng S
tock
Num
ber
Wei
ght
Wei
ght
Wei
ght
Cod
e*N
umbe
r
TO 00-85-20
3-8
Tab
le 3
-1.
Tra
ilers
- C
onti
nued
Nat
ion
alD
imen
sio
ns
Sto
ckP
art
(Les
s D
raw
En
gin
eD
evic
eG
ross
Sh
ipp
ing
En
gin
eN
um
ber
Nu
mb
erB
ar)
Wei
gh
tW
eig
ht
Wei
gh
tC
od
e*J7
5-19
8145
-00-
664-
P117
8421
4x70
x79
5155
5056
1021
195
58
J75-
19A
/B81
45-0
0-62
6-P1
3327
214x
70x7
973
050
5657
8636
81
J75-
1781
45-0
0-66
4-P1
1784
214x
70x7
951
5550
5610
211
9558
J57-
17A
/B81
45-0
0-62
6-P1
3327
214x
70x7
973
050
5657
8636
81
J79-
1181
45-0
0-78
5-70
36R
41G
417
0x64
x65
3150
2880
6030
4808
J79-
1181
45-0
0-59
0-10
5R20
0G4
170x
64x6
531
5028
8060
3048
54
J79-
1581
45-0
0-78
5-10
5R20
0G4
170x
62x7
531
5029
0060
5048
11
En
gin
eN
atio
nal
Par
tD
imen
sio
nE
ng
ine
Dev
ice
Gro
ssS
hip
pin
gS
tock
Nu
mb
erN
um
ber
(Les
s D
raw
Wei
gh
tW
eig
ht
Wei
gh
tC
od
e*B
ar)
J85-
5, 1
381
45-0
0-04
4-69
99T
14G
0170
x42x
4644
861
010
5888
58
J85-
5, 1
381
45-0
0-92
9-37
E50
1460
66x4
0x44
484
859
1058
9454
J85-
5, 1
381
45-0
0-99
4-37
E50
1460
66x4
0x44
448
859
1058
3823
J85-
581
45-0
0-98
8-59
99T
20G
0211
7x40
x41
584
275
859
3676
J85-
781
45-0
0-99
4-37
E50
1460
66x4
0x44
428
610
1038
3822
G00
1
J85-
17,1
7A81
15-0
0-25
1-69
99T
03G
0164
x40x
4642
861
010
3894
95
J85-
1781
45-0
0-00
5-60
x41x
4142
820
062
887
44
J85-
2181
45-0
0-03
2-69
99T
2773
x40x
4552
070
012
2067
05
TO 00-85-20
3-9
Tab
le 3
-1.
Tra
ilers
- C
onti
nued
Nat
ion
alD
imen
sio
ns
Sto
ckP
art
(Les
s D
raw
En
gin
eD
evic
eG
ross
Sh
ipp
ing
En
gin
eN
um
ber
Nu
mb
erB
ar)
Wei
gh
tW
eig
ht
Wei
gh
tC
od
e*G
01
J100
CA
100
8145
-00-
146-
7140
235
74x4
0x43
430
705
1135
3829
T53
-L13
8145
-00-
772-
8115
CO
NO
24-3
75x4
0x43
550
657
1207
7870
T56
AL
L81
45-0
0-55
0-68
0020
117
6x51
x61
1326
259
1585
7451
T56
AL
L81
45-0
0-66
1-68
0030
239
x22x
1654
834
389
129
72
8145
-00-
887-
6900
399-
2544
x40x
4054
840
295
019
49
0-09
650-
23
T56
AL
L81
15-0
0-52
6-68
0008
439
x22x
1660
170
230
2868
TO
RQ
UE
ME
TE
R
T56
-7,
981
15-0
0-66
3-68
0008
311
1x46
x50
1240
383
2624
9802
8145
-00-
687-
6800
216
111x
46x5
012
4038
326
2481
10
8145
-00-
839-
6854
347
126x
52x6
112
4015
4527
8584
18
8145
-00-
888-
6800
444
126x
52x6
112
4015
4527
8536
98
T56
-981
15-0
0-04
9-68
0008
711
1x46
x50
1123
1500
2623
5204
T56
-15
8145
-00-
839-
6854
347
126x
52x6
113
2615
4528
7184
18
T56
-15
8145
-00-
888-
6800
444
126x
52x6
113
2615
4528
7136
98
T40
0-C
P400
8145
-00-
465-
3018
391
68x3
4x50
708
600
1308
6474
T40
0-G
B40
081
45-0
0-46
5-30
1839
252
x36x
3345
035
080
063
73
T76
8145
-00-
832-
8694
40-1
64x4
6x45
322
345
667
9706
TO 00-85-20
3-10
Tab
le 3
-1.
Tra
ilers
- C
onti
nued
Nat
ion
alD
imen
sio
ns
Sto
ckP
art
(Les
s D
raw
En
gin
eD
evic
eG
ross
Sh
ipp
ing
En
gin
eN
um
ber
Nu
mb
erB
ar)
Wei
gh
tW
eig
ht
Wei
gh
tC
od
e*T
F39
RA
W81
45-0
0-86
0-94
09M
9910
4x44
x58
7260
3622
VK
193-
0487
CD
45A
263
TF3
981
45-0
0-99
0-4S
9000
2-10
3A73
5053
07
BU
ILT
-UP
10-3
6081
45-0
0-87
1-SK
1118
,60
x42x
4645
050
095
0SE
RIE
S85
57SK
2100
F100
IN
LE
T81
45-0
0-39
4-P5
0363
55x5
5x43
338
842
1180
FAN
6566
PT
F100
IN
LE
T81
45-0
1-11
6-10
0975
53x5
3x43
338
477
815
FAN
9588
PT
F100
CO
RE
8145
-00-
394-
P491
6710
1x61
x65
1085
1874
2959
2056
PT
F100
CO
RE
8145
-01-
116-
1007
6610
0x62
x63
1085
1387
2472
9587
PT
F100
8145
-00-
394-
P491
3692
x46x
5734
310
4513
88T
UR
BIN
E65
61PT
F100
8145
-01-
116-
1009
9992
x47x
4834
367
610
19T
UR
BIN
E95
90PT
F100
8145
-00-
394-
P497
3511
5x61
x69
453
1590
2043
AU
GM
EN
TE
R65
62PT
F100
8145
-01-
116-
1009
8711
4x62
x67
453
1230
1683
AU
GM
EN
TE
R95
89PT
F100
8145
-00-
394-
P482
2635
x33x
2578
187
265
GE
AR
BO
X66
73PT
F100
8145
-01-
116-
1009
5939
x37x
2978
183
261
GE
AR
BO
X95
86PT
T-5
6 C
OM
P81
45-0
1-20
4-23
0370
1053
x38x
4641
644
085
5M
OD
UL
E73
93A
S
T56
TU
RB
2835
-01-
243-
6870
436
32x3
3x43
405
225
630
MO
DU
LE
3721
TO 00-85-20
3-11
Tab
le 3
-2.
Ada
pter
s
EN
GIN
ET
YP
E A
DA
PT
ER
/ W
EIG
HT
TY
PE
TR
AIL
ER
/WE
IGH
TE
NG
INE
WE
IGH
T/G
RO
SS
WE
IGH
TT
F30P
3N
SN 1
740
00 1
03 0
870Y
Z/2
30#
NSN
174
0 00
580
049
4/75
0 #
4135
/511
5
TF3
0P7
NSN
174
0 00
103
087
0YZ
/230
#N
SN 1
740
00 5
80 0
494/
750
#41
35/5
115
TF3
0P9
NSN
174
0 00
103
087
0YZ
/230
#N
SN 1
740
00 5
80 0
494/
750
#41
35/5
115
TF3
0P10
0N
SN 1
740
00 6
89 4
115P
Q/2
30#
NSN
174
0 00
580
049
4/75
0#41
35/5
115
TF3
3P3
TF3
3P5
NSN
174
0 00
911
102
6/33
0#N
SN 1
740
00 5
54 1
667/
820
#43
00/5
450
TF3
3P7
NSN
174
0 00
911
102
6/33
0#N
SN 1
740
00 5
80 0
494/
750
#47
50/5
830
TF3
3P9
NSN
174
0 00
911
102
6/33
0#N
SN 1
740
00 5
80 0
494/
750
#43
00/5
380
TF3
3P10
0AN
SN 1
740
00 9
11 1
026/
340#
NSN
174
0 00
580
049
4/75
0 #
4750
/584
0
TF4
1A1
NSN
173
0 00
708
794
8CN
/390
#N
SN 1
740
00 7
13 5
908/
730
#31
90/4
310
J57-
19W
NSN
173
0 00
589
946
4/11
0#N
SN 1
740
00 7
13 5
908/
730
#39
70/4
810
J57-
21N
SN 1
730
00 5
73 5
114/
105#
NSN
174
0 00
516
793
0/58
0 #
4615
/530
0
J57-
29W
AN
SN 1
730
00 5
89 9
464/
110#
NSN
174
0 00
713
590
8/75
0 #
3820
/468
0
J57-
43W
BN
SN 1
730
00 5
89 9
464/
110#
NSN
174
0 00
713
590
8/75
0 #
3770
/463
0
J57-
19N
SN 1
730
00 6
57 1
179/
95#
NSN
174
0 00
713
590
8/75
0 #
5155
/600
0
J75-
19W
NSN
173
0 00
657
117
9/95
#N
SN 1
740
00 7
13 5
908/
750
#51
55/6
000
TF-
34N
SN 4
920
00 5
91 6
975/
780#
NSN
174
0 00
713
590
8/75
0 #
1443
/297
3
T-5
6N
SN 1
730
00 2
38 8
019/
262#
NSN
174
0 00
690
518
4/75
0 #
1326
/233
8
J-60
NSN
174
0 00
854
597
2/22
6#N
SN 1
740
00 6
90 5
298/
450
#46
0/11
36
NSN
174
0 00
854
597
3/16
#
J-65
NSN
173
0 00
573
511
5/13
3#N
SN 1
740
00 5
16 7
929/
500
#26
90/3
323
F100
-PW
-220
NSN
814
5 01
050
518
8PT
/802
#N
SN 1
740
00 7
13 5
908/
740#
3085
/456
4
F-10
0N
SN 8
145
01 0
50 5
188P
T/8
02#
NSN
174
0 00
713
590
8/74
0 #
3085
/462
7
F101
-GE
-102
NSN
174
0 01
166
112
7/64
1#N
SN 1
740
00 7
13 5
908/
740
#48
24/6
205
21C
7082
G01
NSN
174
0 01
108
349
5
F110
-GE
-100
NSN
174
0 01
189
416
4/76
5#N
SN 1
740
00 7
13 5
908/
740
3965
/547
0
F110
-GE
-129
NSN
174
0 01
189
416
4/76
5#N
SN 1
740
00 7
13 5
908/
740
3980
/547
0
TO 00-85-20
Table 3-3. Shipping Device Weights
TRAILERS STOCK NUMBER WEIGHT
300 Mod to 1740 00 516 7930 580=
3000E 1740 00 713 5908 730=
3010 1740 00 554 1667 820=
3030 1740 00 580 0494 750=
ADAPTERS
TF30 1740 00 103 0870YZ 230#
1740 00 689 4415PQ
TF33 1740 00 911 1026 330#
TF33 P100 1740 01 008 4348 330#
TF33 P102 1730-00-485-8615 330#
TF34 4920 00 591 6975 780#
TF41 1730 00 706 7948CN 390#
T56 1730 00 238 8019 262#
J57-19/2/9/43WB/59 1730 00 589 9464 110#
1730 00 626 5691 190#
J57-13/21/23/55 1730 00 573 5114 105#
J60 1740 00 854 5972 226#
1740 00 854 5973 16#
J65 1730 00 573 5115 113#
J75 1730 00 657 1179 95#
J79 1730 00 657 1178 150#
F100 8145 01 050 5188PT 802#
ENGINE CONTAINER STOCK NUMBER
T58-3 37D400176P101 8145 00 859 0549
5999T21G01 8145 00 988 3679
T58-5 37D400176G002 8145 00 928 4859
T64-7/7A 5999T05G01 8145 00 111 5843
5999T05G02 8145 00 901 6327
T400-401/402 PK1361 8145 00 486 0245
T53-11/13 8115CON024-3 8145 00 772 7870
F200-23A Fiberglass 100975 8145 01 116 9588PT
Metal P50363 8145 00 394 6566PT
F200-23B Fiberglass P49167 8145 01 116 9597PT
Metal 8145 00 396 2056PT
F200-23C Fiberglass 100999 8145 01 116 9590PT
Metal P49136 8145 00 394 5561PT
F200-23F Fiberglass 100987 8145 01 116 9589PT
Metal P49735 8145 00 394 6562PT
F200-23G Fiberglass 100959 8145 01 116 9586PT
Metal P48226 8145 00 394 6673PT
F200-23H Fiberglass P50689 8145 01 035 1387PT
3-12
TO 00-85-20
CHAPTER 4PREPARATION AND INSPECTION
4.1 GENERAL INFORMATION.
4.1.1 This section provides information and instructions for the protection, preparation and inspection of Air Force enginesfor shipment. Preservation procedures are prescribed in TO 2J-1-18, TO 2R-1-11, and appropriate engine handbooks.
4.1.2 Engines designated for surface shipment shall be prepared for 1 to 180 days storage and engines designated for airshipment shall be prepared for over 180 days storage in accordance with TO 2J-1-18 or TO 2R-1-11.
NOTE
Extreme caution must be exercised to insure that all engines are drained of residual fuel and all drains are sealed.Flight safety of aircraft is seriously affected by drainage or residual fluids during shipment.
4.1.3 TF33 Engine. Position engine with large fan section to rear of trailer.
4.1.4 TF41 Engine. Position engine with top yoke frame member on front of trailer.
NOTE
Jet engines are not authorized for rail shipment unless approved by Item Manager and DSPP office at primeALC. Approved for rail shipment is sometimes granted for engines being transported for salvage or otherconsiderations to warrant rail movement.
4.2 REQUIRED DOCUMENTS AND ENTRIES.
4.2.1 Verify engine is prepared for shipment with the following entry made in the REMARKS section of the ConsolidatedEngine Management System (CEMS) A295, automated history program database:
Engine prepared for shipment in accordance with TO 2J-1-18, date, inspectors name and/or stamp.
4.2.2 Engines designated for airlift will require certification on DD FORM 1387-2 that the engines have been prepared andpackaged in accordance with the applicable technical order and all certification requirements of AFMAN 24-204 have beenaccomplished. Certification of proper preparation, packaging, and marking is generally accomplished by transportationpersonnel. These individuals are authorized in writing to accomplish the DD FORM 1387-2 by virtue of attending a DoDhazardous materiel school. No person may perform duties and responsibilities for preparing and certifying engines unless hehas satisfactorily completed that training.
NOTE
Above requirements do not apply to maintenance technicians.
4.2.3 Engines prepared for shipment on trailers, trucks, stands or dollies shall be tagged with AFTO FORM 81 or identifiedwith the following markings on the wrapping on each side of the engine in two-inch high letters using red ink conforming toFederal Specification TT-I-558:
4.2.4
CAUTION
DELICATE AIRCRAFT ENGINE.HANDLE WITH CARE DURING MOVEMENT/LOADING/OFF LOADING.
Change 4 4-1
TO 00-85-20
When shipment of an engine is made on a stand, skid, trailer or in a container, the shipping device(s) will be listed on a DDFORM 1348-1 and accountability will be transferred to the accountable officer at destination. If an activity receives a trailer,stand, skid or adapter on a DD FORM 250 from a contractor, the receiving activity will handscribe a DD FORM 1348-1 forinput to the base accountable record and pick up accountability for the trailer, stand, skid or adapter.
4.2.5 The shipment of any aircraft engine requiring air ride equipment for surface movement will be identified byannotating the supplemental information block of DD FORM 1387-2 to read “Surface via air ride vehicle required inaccordance with TO 00-85-20.”
4.3 PREPARATION FOR SHIPMENT.
The following sections will define procedures and policy depending upon what device is used and the mode of shipmentselected for transporting engines. Special instructions for the T76 engine are also included.
4.4 SHIPMENTS ON TRANSPORTATION TRAILERS, SKIDS OR DOLLIES.
CAUTION
Under no circumstances should standard commercial hardware be used to fasten the engine support brackets tothe engine or trailer. Use of lower strength hardware than specified could cause serious engine damage duringshipment and handling.
NOTE
• Engine trailers shall be inspected prior to movement of engine for bent tie rods, tire condition and correct PSI,all locking pins in place, tow bar condition and check of front axle for cracks, broken welds and alignment.Adapter assemblies such as used on TF41 engines shall be stenciled: DO NOT REMOVE WHILE ENGINEIS BEING TRANSPORTED. Use red paint conforming to Federal Specification TTOP-37C or equivalent.The letters shall be one inch if room permits; if not, paint the letters at least 3/4 of the surface size beingpainted. Removal of this equipment while in transit has resulted in engines being damaged. All engineopenings will be closed in accordance with section IV, TO 2J-1-18.
• Shipping of engines using transition or installation equipment adapters are prohibited. Only transportationadapters with tie down provisions for surface shipment are permissible.
• The Transportation Officer should notify trucking companies when ordering trailers that only wood beds areacceptable as the Air Force has no available means of tying down to metal beds, trailers, or trucks.
4.4.1 Engines mounted on trailers, trucks, stands or dollies shall be protected from the elements and foreign matter by acover or shroud. The cover or shroud will be designed and/or installed in such a manner that it will also serve as a leakagereceptacle which will trap any residual fluid leakage from the engine. Barrier material will be placed on the engine atnecessary points to prevent the engine cover or shroud from tearing on sharp protrusions. (Optional material which can beused in MA4050, NSN 9330-01-308-5153.)
NOTE
Since it is virtually impossible to eliminate seepage from preserved engines, it has become necessary to includean absorbent material under the engine wrap next to engine to absorb fluid leakage. The material to be used is T-500, NSN 9330-01-334-3304. This will eliminate air aborts as a result of leakage during airlift (TO 2J-1-18,section VIII).
4.4.1.1 All unpurged engines on trailers will have a first wrap of conductive material such as MIL-B-81705, type II, NSN9330-00-113-9438 (500 foot roll), or MIL-P-82646 (not stocklisted). This will replace L-P-378 that is most commonly usedas the first wrap. Additional wraps and barriers will continue as at present.
4-2
TO 00-85-20
CAUTION
We emphasize that the use of conductive wrap on unpurged engines is to minimize the risk of ignition. Under nocircumstances is this a substitute for properly purging engines.
4.4.1.2 Covers of shrouds will be installed on trailer mounted engines in the following preferred order:
4.4.1.2.1 Flexible environmental control containers, conforming to MIL-C-9959 (reusable) (Figure 4-2) or MIL-C-58104(AV).
4.4.1.2.2 Shroud type covers. Materials suitable for shrouding engines are 0.004 inch (4MIL) polyethylene (specificationMIL-P-3803) and vinyl coating glass fibre laminated material (open weave) or equivalent (Figure 4-3). Shroud type coversare the least preferred methods of protecting engines and use of the shroud will be limited to shipments where inside orcovered storage/transport provides a degree of environmental control beyond that offered by the shroud. Shrouds are notintended for use as engine storage containers and shall be restricted in use from 45 to 180 days.
4.4.2 Engines prepared for air shipment.
4.4.2.1 Engines for air shipment will be purged in accordance with TO 2J-1-18 or TO 2R-1-11.
4.4.2.2 Airlift, whenever feasible, will be the preferred mode of transportation for trailer mounted engines.
4.4.2.3 See Chapter 6 for additional instructions on tiedowns.
4.4.3 Engines prepared for truck shipment.
4.4.3.1 Engines for truck shipment will have their fuel systems purged in accordance with TO 2J-1-18 or TO 2R-1-11.
4.4.3.2 Truck shipments of engines mounted on airlift trailers will be tied down as follows:
4.4.3.2.1 Position trailer parallel with truck bed. Recommend towbar faces aft for ease of off loading.
4.4.3.2.2 Apply brakes.
4.4.3.2.3 Be sure rail clamps on roller adapters are tight (Table 4-2).
4.4.3.2.4 Position tiedown chains or cables to avoid contact with each other, parts of the engine, or trailer to preventchafing.
4.4.3.2.5 Maintain lowest or smallest possible angle between floor and tiedown chain, 45° or less.
4.4.3.2.6 Position wood chocks in accordance with Chapter 6.
4.4.3.3 Engines on dollies will not have the wheels raised permitting the dolly frame to rest on the floor.
4.4.3.4 Engines shipped on open type carrier equipment shall be covered with tarpaulins which will protect the enginesfrom the weather elements. The tarps will be installed and fastened in a manner which will prevent vibrations and flappingduring movement.
NOTE
T58 engines may be shipped on trailers with QEC kit installed.
4.4.3.5 Trailer mounted engines will not be shipped on “Hot Shot” equipment (pickup vehicles with fifth wheel goosenecktype hook-up), pulling a mini trailer. Pickup vehicles with improved commercial type truck and trailer hook-ups areacceptable.
4-3
TO 00-85-20
NOTE
Fragile external components will be protected from damage due to tarpaulins by the use of fiberboard blocks,rigid plastic foams, wood, etc.
4.4.4 Rail and Ocean Transportation of Trailer Mounted Engines
4.4.4.1 The following engines are approved for limited ocean transportation when prepared for shipment per steps 4.4.4.2.1through 4.4.4.2.3. Limited ocean transportation is defined as less than 72 hours of over water transportation from engineloading to unloading. Wrapped engines will be transported over water only in an enclosed air-ride truck or trailer. Enclosedair-ride trucks or trailers with turbine engines will not be crane loaded onto ocean transport. Air-ride trucks or trailers will bedriven onto ocean transportation. Consult appropriate engine technical data for limits and on condition maintenancerequirements for engines that have been exposed to excessive humidity during over water transportation.
4.4.4.1.1 F100 series engines
4.4.4.1.2 F110 series engines
4.4.4.1.3 TF33 series engine
4.4.4.1.4 T56 series engine
4.4.4.1.5 F101 series engine
4.4.4.1.6 F118-100 series engine
4.4.4.1.7 F108 series engine
4.4.4.1.8 J85 series engine
4.4.4.1.9 J69 series engine
4.4.4.1.10 T34 series engine
4.4.4.1.11 T64 series engine
4.4.4.1.12 T400 series engine
4.4.4.1.13 T700 series engine
4.4.4.1.14 T53 series engine
4.4.4.2 Wrapping procedures per paragraph 4.4.3 will be used, with the following additions.
4.4.4.2.1 A locally procured plastic container will be used to hold 1000 units of desiccant. The container will hold thedesiccant and prevent desiccant contact with all engine parts. Desiccant will be placed inside the container, in the enginetailpipe immediately prior to engine wrapping. Desiccant containers may be reused.
4.4.4.2.2 Engine wrapping will be conducted as rapidly as possible to insure minimal desiccant exposure to humidity duringthe wrapping process.
4.4.4.2.3 A humidity indicator will be visibly mounted on the engine. The humidity indicator will be visible after the finalwrap of the engine. The humidity indicator will be an MS20003 Humidity Indicator or functional equivalent. The humidityindicator will have a visible color change for varying levels of humidity. The humidity indicator will be attached to thewrapped engine prior to the final wrap with plastic.
4.4.4.3 Rail transportation of trailer mounted engines is prohibited.
4.4.4.4 Ocean transportation of trailer mounted engines not listed in paragraph 4.4.4.1 is prohibited.
4.4.5
4-4 Change 4
TO 00-85-20
CAUTION
• Pneumatic suspension (air ride) is a suspension system that utilizes air bags and does not have springs (seeFigure 4-3). Failure to comply with this requirement may result in damage to engine bearings and other vitalengine components.
• When preparing the F108 engine for surface shipment, ensure no tie downs cross over any portion of thecradle and shock mount assembly. Any tie down attached to or which passes over cradle and shock mountwould eliminate shock dampening feature and result in engine bearing damage.
All Air Force jet engines, which are transported on Air Force 3000 or 4000 series trailers (48 inch rail “fly away”) during“off base” surface transportation, will require air ride tractor and trailer. A medium duty truck, (one piece chassis) with frontand rear air ride suspension, is suitable for transportation of trailer mounted engines. Any engine which utilizes a specialtrailer, such as the ETU-111E (F108 engine), will require air ride shipment. Transportation cans/containers which have shockor spring protection included will not require air ride equipment.
4.5 SHIPMENTS IN ENGINE CONTAINERS (STEEL, REUSABLE).
Table 4-1 lists container pressure changes which will occur due to temperature variations. The pressure-versus-temperaturetable should be used during leak checks to correlate pressure changes resulting from temperature variations.
4.5.1 General.
4.5.1.1 Canned engine movement is authorized when transportation trailers are not available or the circumstances warrantshipment in a container.
4.5.1.2 Engine fuel systems must be purged in accordance with TO 2J-1-18 or TO 2R-1-11 prior to being containerized.
4.5.1.3 Containers will be pressurized with dry nitrogen in accordance with TO 2J-1-18.
4.5.1.4 Prior to shipment the container will be pressure checked to ascertain if it is inerted.
NOTE
Containers that were not designed for pressurization will not be used for air shipment.
4.5.1.5 Procedure for pressure checking metal engine container: The engine cans will be checked by transportationpersonnel for pressure within 24 hours of shipment or trans-shipment using a low-pressure air gauge such as NSN 4910-00-800-8899; cans which have less than 1 psig or do not meet Table 4-1 will be turned over to maintenance for processing inaccordance with TO 2J-1-18 or TO 2R-1-11.
Change 4 4-4.1/(4-4.2 blank)
TO 00-85-20
4.5.2 Engines prepared for air shipment. No special procedures or tiedown instructions are required for air shipments incontainers other than to insure preservation and pressurization procedures in TO 2J-1-18 or TO 2R-1-11 are complied with.
4.5.3 Engines prepared for truck shipment.Engines transported by trucks in metal containers will be tied down the same asFigure 6-7 and Figure 6-8 in accordance with Chapter 6. Specialized carrier equipment (i.e., low-boy or drop well trailers) isauthorized for transporting full engine containers double-decked and when proper tiedown procedures are applied.
4.5.4 Preparation for rail shipment. Engines are authorized for rail shipment when installed in metal containers and preparedas follows:
4.5.4.1 Wood skids blocked at each end by nailing a 2 x 4 block (or larger) to the deck with 20 penny nails. A second set ofblocks (2 x 4) will be nailed on top of the first set of blocks. Blocks will be a minimum of 18 inches long.
4.5.4.2 Containers will have a minimum of two each steel bands, two inches wide, over the top of the containers. Strappingwill conform to QQ-S-781, type 1, class A, Figure 6-7 and Figure 6-8.
4.5.4.3 Anchor plates, NSN 5340-00-252-3014 or NSN 5340-00-252-3015, as applicable, will be used to secure strappingto deck as required. Plates shall be secured to deck with gimlet points, round head screws, NSN 5306-00-307-7685.
4.5.5 Preparation for ocean shipment. Engines to be shipped via ocean transportation shall be prepared in completecontainers. Skids, trailers, dollies or stands shall not be used for shipment of aircraft engines via ocean transportation.
4.5.6 Accident engines and/or engines designated for TDRs.
4.5.6.1 Engines removed from aircraft involved in accidents, wherein engine failure or malfunction was known or suspectedto be a factor in the accident, require special handling and shall be prepared for shipment in accordance with applicablecontainers used in shipping accident engines or accessories for priority disassembly and inspection. A red band eight incheswide will be brush or spray painted horizontally around the container, immediately above the opening flange. Accessorycontainers will have the band painted where convenient. Upon removal of the accident engine or accessory, the red band willbe obliterated immediately and necessary painting accomplished to return container to original finish.
Table 4-1. Container Temperature vs. Nitrogen Pressure
TEMPERATURE PRESSURE TEMPERATURE PRESSURE°C °F PSIG °C °F PSIG60.0° 140° 7.6 4.4° 40° 3.9
54.4 130 7.3 -1.1 30° 3.5
48.9 120 6.9 -6.7 20° 3.2
43.3 110 6.5 -12.2 10° 2.8
37.8 100 6.1 -17.8 0° 2.4
32.3 90 5.8 -23.3 -10° 2.0
26.7 80 5.4 -18.9 -20° 1.7
21.1 70 5.0 -34.4 -30° 1.3
15.6 60 4.6
10.0 50 4.3
NOTE
A plus and/or minus of 1.0 psig is permissible for transportation check point acceptability.
4-5
TO 00-85-20
Figure 4-1. Engine in a Flexible Environmental Container
4-6
TO 00-85-20
4.5.6.2 For engines which do not have metal containers, a fully serviceable environmental container will be used. Aconspicuous form of identification marking will be used to distinguish an accident TDR engine.
NOTE
• The aft engine transportation yoke (strong back) (NSN 4920-00-960-4678) is equipped with mooring ringswhich are satisfactory for mooring aft end of engine during shipment. Front of engine will be moored bylooping restraining chains around forward cradle adapter blocks adjacent to trailer rails. Pass chain throughopening between upper end of cradle (part number 1C5277-1G1) and support assembly (part number 1C5277-3G1) (TO 35DA3-6-20-1, figure 10-2). Insure chain is routed under turnbuckle (part number 1C5277-3P19).Opposite end of chains should then be secured to aircraft decking directly forward of engine.
• To support mission requirements of AAC forward operating locations for air transport of fully equipped andtested J79 engines for requirements to support the AAC assigned F-4F aircraft undergoing programmed depotmaintenance (PDM) the 4100 rail system on 3000 series trailers, with multipurpose adapter assemblies (NSN4920-00-960-4676) and transportation yokes (strong backs) (NSN 4920-00-960-4678) may be used wheneverairlift is required of J79 engines with afterburners and quick engine change (QEC) kits installed.
4.5.7
CAUTION
Unless specified in applicable engine technical manuals, when tightening the flange bolts, work at first on oneside, then on the other and apply less than full torque in working around the flange the first time. The use ofgrease or oil as an additional sealant should be avoided as permanent damage to the rubber flange seal will result.
Attach a suitable sling to the lifting eye in the top section of the container method “LIFT HERE” and lower the top section inplace on the lower section with the aid of two long drift pins, one at each end of the cover. Install the closure bolts and drawdown evenly. The final torque will be determined by torque values established for the bolts used (Table 4-2).
4.6 SHIPMENTS IN ENGINE MODULE CONTAINERS (STEEL AND FIBERGLASS REINFORCED PLASTIC
(FRP), REUSABLE).
Pressurization requirements apply only to containers for built-up engines which may contain residual fuel. As all fuel isremoved from engine modules during the disassembly process, pressurization requirements do not apply to steel and FRPengine model containers.
4.6.1 General.
4.6.1.1 Engine module containers are not designed to be pressurized containers. The containers will be at or near zeropressure because the relief valves will immediately release any build-up of pressure or vacuum.
4.6.1.2 On first loading of the engine module into the container or after a major repair of the container, a slightpressurization (maximum 0.75 PSI) with air may be warranted. The purpose of the pressurization would be to determine theoverall seal integrity of the container.
4.6.1.3 The preparation of engine modules for shipment by the various transportation modes is the same as that required forbuilt-up engines, except that the pressurization requirements of TO 2J-1-18 do not apply.
4.7 SHIPMENTS IN WOOD BOXES.
Wood boxes are not recommended and should be used only when other types of shipping devices are not available. Whenused, they shall comply with MIL-C-4116 and TO 2J-1-18.
4-7
TO 00-85-20
Figure 4-2. Tie Down Diagram for Airlift Trailers Transported on Trucks
4-8
TO 00-85-20
Table 4-2. Recommended Torque Values for Container, Trailer and Adapter Bolts
Bolt or Nut Size Torque Value/Inch-Pounds8-36 12-15
10-32 20-25
1/4-28 50-70
5/16-24 100-140
3/8-24 160-190
7/16-20 450-500
1/2-20 480-690
9/16-18 800-1000
5/8-18 1100-1300
3/4-16 2300-2500
7/8-14 2500-3000
1-14 3700-5500
1-1/8-12 5000-7000
1-1/4-12 9000-11000
8-32 12-15
10-24 20-25
1/4-20 40-50
5/16-18 80-90
3/8-16 160-185
7/16-14 235-255
1/2-13 400-480
9/16-12 500-700
5/8-11 700-900
3/4-10 1150-1600
7/8-9 2200-3000
NOTE
The above torque loads may be used for all cadmium plated steel nuts of the fine or coarse thread series whichhave approximately equal number of threads and equal face bearing areas.
4-9
TO 00-85-20
Figure 4-3. Pneumatic Suspension (Air Ride) Truck and Trailer (Typical) (Sheet 1 of 2)
4-10
TO 00-85-20
Figure 4-3. Pneumatic Suspension (Air Ride) Truck and Trailer (Typical) (Sheet 2)
4-11
TO 00-85-20
4.8 SHIPPING OF ENGINES WITH INSTALLED AFTERBURNERS.
4.8.1 Surface transportation. Unless operational commitment dictates otherwise, afterburner engines shall not be shippedwith afterburners installed. If afterburners is installed, all engines shipped will be via ride truck and air ride trailer. Enginesshipped by this method shall be verbally cleared by Oklahoma City ALC/DSTR, Autovon 339-7751 and have DD FORM1348-1 so annotated. If an F100-PW-220 engine is found not to have been transported on an air ride tractor trailer, the propermanagement office (ASD or SA-ALC) must be contacted to determine if maintenance/inspection will be required or continueengine in service.
4.8.1.1 J85, F100 and F110 series engines are exempt from this requirement.
CAUTION
Failure to ensure proper mounting and related road conditions will result in damage to vital engine components.
4.8.1.2 In the event off-base surface movement of engines with afterburner installed, due to geographical location of testcell or other situation, it is imperative that extreme caution be exercised regarding speed, road conditions, tie down methods,etc. Engines prepared for shipment with afterburner installed shall be properly located on the trailer to ensure the center ofgravity is well forward of the rear axle (preferably at midpoint between front and rear axles if possible).
NOTE
• Air ride tractor-trailer or medium duty truck (one piece chassis) with front and rear air ride suspension isrequired for off-base surface transportation of F100 and F110 series engines.
• J79 engines may be shipped by surface transportation with A/B installed by utilizing 4100 trailers rail on a3000F trailer using adapters in accordance with TO 35-1-8, figure 2-59.
• When applicable, engine may be shipped with QEC kit installed.
• TF30 engines with afterburners installed may be transported by air ride tractor-trailer as an alternate means oftransportation within a 300 mile radius of point of embarkation.
4.8.2 Air Transportation. Engines may be shipped by air with afterburner if:
4.8.2.1 Engines are located well forward on trailer to obtain best center of balance location between axles.
4.8.2.2 Tiedowns are limited on lateral distance to prevent rail spreading.
4.8.2.3 All tiedowns have as nearly equal tensions applied as is possible.
NOTE
F100 and F110 engines may be shipped with the engine positioned on truck with aft end of engine to front oftruck.
4.9 INSPECTIONS.
4.9.1
WARNING
Prior to shipment. Failure to insure the installation of the aft and forward engine adapters safety pins duringshipment, storage, or removal of aircraft engines will cause damage to aircraft equipment and possible injury topersonnel.
4-12 Change 3
TO 00-85-20
Inspection shall be made before shipment of engine shipping devices and protective covering for obvious damage, cracks,corrosion, and general appearance. Transportation officers are authorized to refuse engines and/or shipping devices offeredfor shipment when evidence of above damage is noted.
4.9.2 General cargo will not be placed or stacked against engines during handling, storage, or shipment. The space under theengines can be utilized during shipment via surface and air for compatible type cargo. Extreme caution must be exercisedwhen using this space under the engines to ensure that cargo is properly placed and secured to the pallet of floor of aircraft orcommercial trailer. The tie-down of this cargo must be inspected by the loading supervisor or shipping foreman prior torelease. A minimum of six inches of clearance must be maintained between the bottom of engine and shipping conveyance.
4.9.3 Correction of Deficiencies. When shipment has been damaged (seals broken or open; containers dented or punctured;dehydrating agent discolored) or sub-standard conditions are present, comply with Chapter 2.
4.10 ENGINE RECORDS.
4.10.1 Container shipments. Engine historical records shall be placed in receptacle provided.
4.10.2 Trailer shipments. The waterproof pouch marked “Engine Records Enclosed” shall be folded flap of pouch towardfront of trailer thus preventing entrance of water. Secure pouch to rail with specification PPP-T-97 or PPP-T-60 tape.
4.11 SHIPMENT OF J79 ENGINES WITH AFTERBURNER AND QUICK ENGINE CHANGE (QEC) KIT
INSTALLED ON TRAILER.
4.11.1 Air Transportation. Whenever airlift is required of J79 engines with afterburners and Quick Engine Change Kitsinstalled, the 4100 rail system on 3000 series trailers, with multipurpose adapter assemblies (NSN 4920-00-960-4676) andtransportation yokes (strong backs (NSN 4920-00-960-4678)) may be used, provided:
4.11.1.1 Engines are located well forward on trailer to obtain best center of balance.
4.11.1.2 Tie downs (Figure 4-4) are used.
4.11.1.2.1 Front tie downs require chains to be looped on both sides of adapter around rail.
4.11.1.2.2 Rear tie downs require chains through eyelet on yoke and additional chains looped around yoke on both sidesabove adapter.
4.11.1.2.3 Chafing pads consisting of aluminum strips or other durable material or wrapping of chain with tape at point offriction on trailer rail will eliminate scarring of rail.
4.11.1.3 Tie downs are limited on lateral distance to prevent rail spreading.
4.11.1.4 All tie downs have as nearly equal tension applied as possible.
4.12 F101-GE-102 ENGINE DEVIATIONS TO SHIPPING INSTRUCTIONS.
4.12.1 Engine will be shipped with augmentor (A/B) installed. Shipments may be either one (1) or two (2) engines pervehicle.
4.12.2 The engine and adapter shall only be supported on a 3000E trailer during shipping.
4.12.3 Shipment shall only be via air ride truck and trailer.
4.12.4 The forward engine adapter mounts will be tied down using the criss-cross method (right side chained to the left sideof the flat bed trailer and the left mount chained to the right side of the flat bed trailer) at 20 degrees to 30 degrees forwardlocation of engine. The rear end of the engine adapter will be tied down in the trapezoidal configuration. See sketches for oneand two engine shipments. Roller assemblies shall be rail locks tightened with a square drive bar wrench. Verify forwardtorqued to 65 foot lbs.
4.12.5 Tire Inflation. The tires on the 3000E trailer should be inspected prior to shipment. Tire pressure shall be 30 PSI +5or -0 PSI. Suspect tires should be repaired or replaced. The transporter should be required to inspect the tires periodicallyduring the trip. A flat tire during shipments can cause the engine to become unserviceable.
4-13
TO 00-85-20
4.12.6 See Figure 4-5 and Figure 4-6.
4.13 F118-GE-100 ENGINE DEVIATIONS TO SHIPPING INSTRUCTIONS.
4.13.1 Shipments may be either one (1) or two (2) engines per vehicle.
4.13.2 Engines which have TCTO 2J-F118-517 complied with can be shipped using either adapter, P/N 3C3658 or P/N3C3528G01, with the 3000E trailer. Engines which do not have TCTO 2J-F118-517 complied with shall use adapter, P/N3C3528G01, only for supporting engine for shipment using 3000E trailer.
4.13.3 Ground shipment shall be via air ride truck and trailer only.
4.13.4 Tie down shall be trapezoidal configuration for one (1) and two (2) engine shipments (Figure 4-7 and Figure 4-8).
4.13.5 Tire Inflation. Tires on the 3C3658 trailer shall be inspected prior to shipment. Tire pressure shall be 30 PSI +5 or -0PSI. Suspect tires should be repaired or replaced. The transporter should be required to inspect tires periodically during thetrip. A flat tire during shipment can cause engine to become unserviceable.
4.13.6 See Figure 4-4 and Figure 4-8.
4.14 F118-GE-101 ENGINE DEVIATIONS TO SHIPPING INSTRUCTIONS.
4.14.1 Shipments may be either one (1) or two (2) engines per vehicle. No additional freight authorized when shipping aF118-101 Engine. An exclusive/dedicated tractor-trailer must be used.
4.14.2 The engine and adapter shall only be supported on a 75GH109 transportation trailer during shipment.
4.14.3 Ground shipment shall only be via air ride truck and trailer.
4.14.4 Tire Inflation. Tires on 75GH109 transportation trailer shall be inspected prior to shipment. Tire pressure shall be 30PSI +5 PSI or -0 PSI. Suspect tires should be repaired or replaced. The transporter should be required to inspect tiresperiodically during the trip. A flat tire during shipment can cause engine to become unserviceable.
4-14 Change 6
TO 00-85-20
Figure 4-4. Tie Down Diagram for Air Lift of Trailer
4-15
TO 00-85-20
Figure 4-5. Two Engine Tie Down
4-16
TO 00-85-20
Figure 4-6. One Engine Tie Down
4-17
TO 00-85-20
Figure 4-7. Two Engine Tie Down
4-18
TO 00-85-20
Figure 4-8. One Engine Tie Down
4-19/(4-20 blank)
TO 00-85-20
CHAPTER 5ENGINE AND SHIPPING DEVICE HANDLING
5.1 EQUIPMENT.
5.2 General selection of proper Material Handling Equipment and aids for handling engine during ON and OFF loadingoperations is important to prevent damage to engines and their protective covers.
5.2.1 Use of platform and fork extensions in conjunction with forklifts or side loader trucks is necessary for safe andeffective engine handling.
5.2.2 Under no circumstances will an engine sling be used to transport or lift an engine that is installed in an airlift trailer,half engine container, or engine dollie.
5.3 HANDLING ENGINES IN METAL AND FRP CONTAINERS BY FORKLIFT.
5.4 Forklifts used to handle engines in metal or FRP containers must have a lifting capacity equal or greater than the grossweight of engine and container. GROSS weights will be obtained from Chapter 3 of this Technical Order and forkliftcapacity will be found on forklift nameplate.
5.5 Horizontal containers shall be handled from the side. When lifting containers by forklift, the prongs shall be longenough to fully catch the support rail on the opposite side of the container. Prongs should be spread wide to prevent tippingor tilting of engine container. The outer end or tip of prongs should be tilted upward to prevent engine from slipping off.
5.6
CAUTION
When engine container and engine must be moved after the container top has been removed, DO NOT lift engineand container half by engine hoist fittings as serious damage may result.
The center of gravity (center of balance) of a container with engine installed is indicated on the side of the container. Forkliftprongs shall be positioned equidistant from this “CG” marking before lifting.
5.7 A safety chain from engine to forklift should be used when moving engines by forklift.
5.8 Forklifts will NOT be used to raise airlift trailers with engine installed. When terminal loading ramps are not available,a suitable pallet or bridge, of sufficient strength and dimensions to adequately support the engine, shall be used.
5.9
CAUTION
Extreme care must be taken in handling the TURBOFAN engines due to the circumference of the intake area.This is especially necessary when using a tug or tractor to tow or to back an engine mounted on a trailer to assurethat tow bar does not damage the large fan.
When handling turbofan engines, extreme care shall be used to prevent damage to the turbofan are by the trailer tow bar.Raising of the tow bar during loading or off loading can result in damage sufficient to require overhaul before use of engineis possible.
5-1
TO 00-85-20
5.10 HANDLING ENGINES ON DOLLIES OR TRAILERS.
5.11 The safest method of loading engines which are mounted on dollies or trailers is from a loading ramp. Push theengine dolly or trailer onto the shipping vehicle by use of a forklift or tug using a bridge or platform to span the gap betweenvehicle and ramp.
5.12 Engine may be loaded by hand when forklift or tug is not available. However, sufficient personnel must be presentfor handling the engine by hand (minimum of four).
NOTE
A supervisor must be present at all times during loading of engine mounted on dollies or trailers. Trailer brakesmust be applied when trailer is not in motion.
5.13 When using an inclined ramp for loading, insure that sufficient clearance exists around engine and to insure thattongue of trailer has sufficient clearance to preclude damage of nose section of engine.
5.14 LOADING F108/MULTI-PURPOSE TRAILER ONTO FLATBED WITH FORKLIFT TRUCK (FIGURE 4-3,
FIGURE 5-1, FIGURE 5-2 AND TABLE 4-3).
5.14.1
CAUTION
Highway transportation of the F108 engine requires use of pneumatic suspension equipped (air ride) truck andtrailer (Figure 4-3 and table 4-3).
Minimum 15K capacity forklift required.
5.14.2 Remove trailer steering tongue from steerable axle. Stow tongue.
5.14.3
CAUTION
Do not rotate engine in trailer with removable forklift tube assembly installed in rear forklift slot. Damage toengine may occur if forklift tube assembly is not properly stowed in front forklift slot.
Remove cradle pin and rotate cradle from level position to forklift position.
NOTE
Forklift and level positions are clearly marked on trailer.
5.14.4 Re-pin cradle.
5-2
TO 00-85-20
5.14.5
WARNING
KEEP TOES CLEAR WHEN LOWERING TRAILER.
CAUTION
• Trailer must be in the forklift position before forklift tube is installed.
• Rear forklift tube assembly must be properly installed during all forklift operations. Failure to adhere to thisrequirement could damage engine/trailer.
Remove rear forklift tube assembly from stowed position and insert tube in rear forklift slot.
5.14.6 Lower Trailer. The procedure for lowering the trailer is as follows:
WARNING
TO AVOID PERSONAL INJURY OR DAMAGE TO THE ASSEMBLY, DO NOT USE FORCE TOREMOVE A WHEEL ASSEMBLY LOCKPIN.
5.14.6.1 Ensure front axle and rear wheel selector valves are set to trailer UP or NEUTRAL position (Figure 5-2).
WARNING
KEEP TOES CLEAR WHEN LOWERING TRAILER.
CAUTION
Both front cylinder rod extensions must be even at all times to prevent damage.
5.14.6.2 Remove four wheel assembly lockpins. If a lockpin cannot be removed easily, set selector valves to trailer UP andpump to apply pressure to cylinder until pin can be removed.
NOTE
The trailer will lower under trailer weight. The rate of lowering is controlled by flow restrictor/check valves.Wait approximately three minutes before raising the trailer to allow the hydraulic fluid to flow through restrictorvalves.
5.14.6.3 Set front axle and rear wheel selector valves to trailer DN.
5.14.6.4 Raise wheel assembly to align holes and insert lockpins through each wheel arm to prevent lowering of wheels.
5.14.6.5 Ensure front wheel pin is installed in upper hole, raising wheel assembly as required.
5.14.6.6 Set selector levers to NEUTRAL position.
5-3
TO 00-85-20
5.14.7
CAUTION
If forklift tines are not inserted 72 inches (3/4 length of tubes) into tubes, damage will occur. When insertingforklift tine into forklift tubes, be careful that binding does not occur. Binding could damage engine/trailer.
Insert forklift tines into forklift tubes at least 72 inches.
5.14.8 Carefully lift trailer and engine onto flatbed.
5.14.8.1 Position single engine at forward end of flatbed just aft of truck axle with forward end of engine (fan) facing thefront of the flatbed trailer.
5.14.8.2 When transporting two (2) engines, position engines so that load is evenly distributed over flatbed and truck axles,with forward end of engine (fan) facing the front of the flatbed trailer.
5.14.9 Back forklift truck away from trailer. Be careful not to bind tines in tubes.
5.14.10
CAUTION
• In order to prevent damage to nose cowl, leave cradle in forklift position to maintain clearance between tiedown chains and inlet cowl.
• Do not rotate engine in trailer with removable forklift tube assembly installed in rear forklift slot. Damage toengine may occur if forklift tube assembly is not properly stowed in front forklift slot.
Remove rear forklift tube assembly and stow in front forklift slot.
5.14.11 Secure trailer front, rear and sides in accordance with paragraph 6.13.
5.15 LOADING F108/STAND (PART NUMBER 856A1200) ONTO FLATBED WITH FORKLIFT TRUCK
(FIGURE 4-3, FIGURE 6-14, FIGURE 6-15 AND TABLE 4-3).
5.15.1
CAUTION
• If forklift tines are not inserted 72 inches (3/4) length of tubes, damage will occur. When inserting forklifttines into forklift tubes, be careful that binding does not occur. Binding could damage engine/stand.
• Highway transportation of the F108 engine requires use of pneumatic suspension equipped (air ride) truck andtrailer (Figure 4-3 and table 4-3)
Minimum 15K capacity forklift required.
5.15.2 Insert forklift tines into forklift tubes at least 72 inches.
5.15.3 Insure transportation wheels are in the up and locked position.
5.15.4 Carefully lift trailer and engine onto flatbed.
5-4
TO 00-85-20
5.15.4.1 Position single engine at forward end of flatbed just aft of truck axle with forward end of engine (fan) facing thefront of the flatbed trailer.
5.15.4.2 When transporting two (2) engines, position engines so that load is evenly distributed over flatbed and truck axles,with forward end of engines (fan) facing the front of the flatbed trailer.
5.15.5 Back forklift truck away from trailer. Be careful not to bind tines in tubes.
5.15.6 Secure trailer in accordance with paragraph 6.14.
5.16 TRANSPORTATION OF JET ENGINES BY TOWING.
5.16.1 Background Information. Because of roadway conditions, railroad crossings, foreign objects, surface roughness ingeneral, and the engineering design of jet engines, necessary precautions will be taken to prevent damage during towing ortransportation operations. The heavy compressor and turbine rotors of the jet engine are supported only by the bearings andcarbon seals, and are subjected to permanent damage by sudden stops/impacts.
5.16.2 Practices to be Observed. Organizational chiefs having vehicle operators who tow jet engines will ensure that theoperators are aware of the necessity for using extreme care in transporting jet engines. The following practices will beobserved:
CAUTION
Prior to movement of J85 series engine on J85 trailers, the engine must be installed on the trailer with the nosedome AFT of the trailer tongue to prevent damage to the dome assembly.
5.16.2.1 Prior to movement of the engines:
5.16.2.1.1 Check for and remove from the tug or tractor and trailers all loose bolts, nuts, washers, or other loose objects.
5.16.2.1.2 Check the tug or tractor hitch and all trailer hitches for security and ensure that tongue assemblies and lockingpins are properly secured.
NOTE
Engines will not be moved unless the tug or tractor and trailer hitches, locking pins, and tongue assemblies are ingood operating condition.
5.16.2.1.3 Check and maintain trailer tire pressure.
5.16.2.1.4 Check to ensure that slow moving vehicle emblems are placed on the left rear of the last engine being towed. Toinstall, use the quick release pin at this location. These emblems will be deployed at all times (day or night) while engines arebeing pulled.
5.16.2.2 Confine speed to 5 miles per hour regardless of the speed limit stenciled on the dolly or posted for the particularroadway.
5.16.2.3 Stop or adjust speed down from the 5 miles per hour limit to compensate for rough roadway conditions such asrailroad crossings, temporary crossovers, and locations where utilities are laid on top of the ground.
CAUTION
• When towing engine down loading ramp, do not turn until engine/trailer is completely off inclined surface.
• A maximum speed of 2 miles per hour shall be maintained for inshop transportation during turning operationsfor the F101 and F110 engines.
5.16.2.4 Approach each stop with precaution to avoid jackknifing of dollies or trailers.
5-5
TO 00-85-20
CAUTION
When towing engine down loading ramp, do not turn until engine/trailer is completely off inclined surface.
5.16.2.5 No more than four trailers, loaded or empty, will be pulled by any tractor. To avoid jackknifing trailer trains, theywill be arranged with the most heavily loaded trailer next to the towing vehicle, the next heaviest second in line, and so on. Ifmovement is required on a building ramp, the “train hookup” will be restricted to three trailers.
5.16.2.6 Maintain a minimum of 8 inches clearance between engine pulled in train to allow for slack in coupling pins,tongue assembly and turns that must be made.
5.16.2.7 Secure attaching pins, bolts, and adapters upon removal of the engine from the trailers. All attaching hardware willbe inspected to ensure serviceability and completeness of threads.
5.16.2.8 Attach a light on the back of the rear engine of all engines being towed during the hours of darkness or poorvisibility.
5.17 ADDITIONAL TOWING INSTRUCTIONS FOR F108 ENGINE/MULTI-PURPOSE TRAILER (ETU-111/E).
5.17.1 Raise Trailer. The procedure for raising the trailer is as follows:
WARNING
To avoid personal injury or damage to the assembly, do not use force to remove a wheel assembly lockpin.
CAUTION
Both front cylinder rod extensions must be even at all times to prevent damage.
5.17.1.1 Remove wheel assembly lockpins.
5.17.1.2 Set front axle and rear wheel selector levers to trailer UP.
5.17.1.3 Actuate hand pumps continuously through full range of travel.
5.17.1.4 Lower wheels until wheel assembly lockpins can be inserted.
5.17.1.5 Install steering tongue from stow position and install lockpins.
5.17.2 Remove rear forklift tube assembly from rear forklift slot and stow in front forklift slot.
5.17.3 Remove cradle lockpin, rotate cradle to level position and insert lockpin.
5.17.4 Check to ensure all loose equipment is secured to, or removed from trailer.
5.17.5 Ensure cargo compartment floor dolly is fully retracted.
5.17.6 Ensure tires are serviceable and inflated to 85-95 psi.
5.18 COMPACT AIRCRAFT SUPPORT PACKAGE.
5.18.1 Fabricate or modify APU/Engine change support according to Figure 5-1, Figure 5-2, and Figure 5-3.
5.18.2 Fabricate tool box support according to drawing in Figure 5-4.
5.18.3 Fabricate tire rack according to drawing in Figure 5-6.
5-6
TO 00-85-20
5.18.4 Procure four (4) extra rail brakes.
5.18.5 Remove rails from two (2) 3000E transportation trailers IAW TO 35D3-3-26-1.
5.18.6 Remove lug nuts from tires and remove tires from wheels on one of the trailers.
5.18.7 Drill four (4) each 1/2 inch diameter holes in each rail as indicated in Figure 5-7 of attached drawings.
5.18.8 Install two (2) of the drilled rails on trailer that tires were left installed on axles.
5.18.9 Disassemble tow bar from front axle and install axle to rear set of holes of assembled trailer with tow bar endpointing forward. (Use bolts removed during disassembly to install into holes that were drilled in rail).
5.18.10 Mount rear disassembled axle to front holes of assembled trailer. (Use bolts removed during disassembly to installinto holes that are drilled in rail).
5.18.11 Mount removed rails to assembled trailer IAW Figure 5-5 of attached drawing using two (2) bolts from transferadapter pins on assembled trailer.
NOTE
Rails are installed upside down.
5.18.12 Load engine onto assembled trailer.
5.18.13 Load spare rear TF34 engine adapter onto assembled engine trailer.
5.18.14 Load spare front TF34 engine adapter onto assembled engine trailer.
5.18.15 Load engine change monorail through the back of assembled trailer. Monorail installed underneath and must beinstalled where one of the holes in the monorail will line up with one of the cross bars for engine adapters. Install cross barthrough hole in monorail to hold monorail in place.
5.18.16 Install APU in APU engine change support (Figure 5-1, Figure 5-2, and Figure 5-3) and load APU engine changesupport onto assembled trailer at the rear of trailer.
5.18.17 Attach engine change hoists to APU engine change support using existing pins for hoists that are removed frommonorail to hold in place.
5.18.18 Load engine change CTK onto APU engine change support.
5.18.19 Load torque wrench onto APU engine change support.
5.18.20 Mount tool box support, Figure 5-4, to front of assembled trailer; use bolts from transfer adapter pins to hold inplace.
5.18.21 Mount two (2) each rail brakes on rails that were assembled in step 11 of procedures.
5.18.22 Strap lateral support bars for engine adapters to installed engine lateral support bars.
5.18.23 Secure tool boxes and torque wrench.
5-7
TO 00-85-20
NOTE
• Weight of assembled trailer with engine, APU, and all equipment is 5600 lbs. Cube is not affected.
• When engine change is required two (2) people can remove equipment from assembled trailer and rebuilddisassembled trailer in approximately 40 minutes. This has been tested at this station and both times tookapproximately this long on both occasions. While this is in progress three (3) people can be disconnectingengine from aircraft.
• Tools required for assembly and disassembly of trailer and equipment are normally contained in compositetool kits. Tools used are: 3/4 X 3/8 dr. socket or 1/2 inch dr., 3/8 or 1/2 in ratchet, 9/16 in socket either driveand 9/16 combination wrench, adjustable jaw wrench and a mallet.
5.18.24 When engine change is required, two (2) people remove equipment and rebuild trailer. Engine removed fromaircraft is then dropped onto trailer being assembled. After engine is installed from other trailer the reverse procedures areaccomplished.
Figure 5-1. Multi-Purpose Trailer - F-108 Engine
5-8
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LEGEND
1. Rear wheel mount hydraulic 12. Steering axle selector valve 23. Main cargo floor dolly right-handpump (PR) cylinder (RD)
2. Rear wheel mount selector 13. Steering axle right-hand cylinder 24. Main cargo floor dolly left-handvalve (RF) cylinder (LD)
3. Rear wheel mount right-hand 14. Steering axle left-hand cylinder 25. Main cargo floor dolly center cyl-cylinder (RR) (LF) inder (CD)
4. Rear wheel mount left-hand 15. Restrictor/check valve 26. Hose (H17)cylinder (LR)
5. Restrictor/check valve 16. Hose (H10) 27. Hose (8)
6. Hose (H15) 17. Hose (H9) 28. Hose (H19)
7. Hose (H1) 18. Hose (H11) 29. Hose (H6)
8. Hose (H2) 19. Hose (H12) 30. Hose (H18)
9. Hose (H16) 20. Hose (H14) 31. Hose (H7)
10. Hose (H4) 21. Cargo compartment floor dolly hy- 32. Hose (H14)draulic pump (PD)
11. Steering axle hydraulic pump 22. Bleed needle valve 33. Hose (H14)(PF)
Figure 5-2. Hydraulic System
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TO 00-85-20
Figure 5-3. APU/Eng Change Support
5-11/(5-12 blank)
TO 00-85-20
Figure 5-4. Tool Box Support
5-13/(5-14 blank)
TO 00-85-20
RAILS.50 GAP BETWEEN RAILS
CAUSED FROM AXLE BOALTSOFLOADED TRAILER
BOLT RALIS TOGETHER USINGPREXISTING HOLES
H9102699
Figure 5-5. Rails
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TO 00-85-20
Figure 5-6. Tire Rack
5-16
TO 00-85-20
43.25TYP
58.25TYP
151.50
.75
A
A
SECTION A–A
RAIL MODIFICATIONDRILL 4 EACH .50 DIA. HOLES
ON CENTER BELOW.OUTSIDE LIP ONLY.
RAIL LENGTH 12’7.5 "
H9102701
Figure 5-7. Rail Modification
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TO 00-85-20
CHAPTER 6TIE DOWN INSTRUCTIONS
6.1 GENERAL.
6.2 The tie down instructions in this section are applicable to engines being shipped by aircraft, surface carrier equipmentincluding vans, flatbed trailers, deep-well trailers and rail shipment.
6.3 This section describes various tie down instructions for several shipping devices in different methods of shipment.
6.4 Figures in this TO depict an approved method of tiedown for the type of equipment illustrated; however, an illustrationof a 2000 pound engine tiedown is not necessarily the same method or equipment which should be used for a 5000 poundengine. Illustrations show an approved method of tie down for a given type of loading unless otherwise noted. Theillustrations used herein are intended to depict approved methods of tie downs for different modes of shipment and may beapplied to all applicable shipments.
6.5 In accordance with ICC regulations and AFMAN 24-201, the responsibility for securing engines on trucks or rail carsrests with the shipping activity. Therefore, before acceptance of any transportation facility for shipping aircraft engines byany method the facility shall be inspected by responsible Air Force personnel to insure that the dock will adequately supportthe engines.
NOTE
The Transportation Officer should notify trucking companies when ordering trailers that only wood beds areacceptable as the Air Force has no available means of tying down to metal beds, trailers, or trucks.
6.6 RAIL SHIPMENT.
6.6.1 Shipment of gas turbine engines loaded on airlift trailers is NOT authorized. Approved engines for rail shipment willbe prepared as follows (Figure 6-7 and Figure 6-8):
6.6.2 Wood skids shall be inspected for good condition and shall be blocked at each end of container by nailing a block ineach position mentioned above. The blocks shall be of 2 x 4 or larger material nailed to the decking by 20 dd nails, a second2 x 4 block shall be nailed on top of the first set of blocks. Blocks shall be at least 18 inches or longer.
6.6.3 In addition to the blocks, containers shall be secured by steel bands across the top of the container. The steel bandsshall be at least two inches wide and each container shall require two each steel bands. Strapping shall conform tospecification QQ-S-781, type I, class A.
6.6.4 Strapping or bands shall be protected at all points where the band passes over sharp edges or around corners, toprevent damage.
6.6.5 Anchor plates, NSN 5340-00-252-3014 or 5340-00-252-3015, as applicable, shall be used for fastening strapping todeck if required to adequately secure the container. Anchor plates shall be secured with gimlet point round head screws.
6.7 AIRLIFT SHIPMENT.
6.7.1 Shipment of airlift trailers of the 2000 and 3000 series containing engines for AIR shipment shall be tied down asfollows (Figure 6-6):
6.7.2 Position trailers on cargo deck.
6.7.3 Apply brakes.
6.7.4 Attach all tie down chains or cables to engine adapters.
Change 4 6-1
TO 00-85-20
6.7.5 Position tie down cables or chains to avoid contact with each other or with any part of engine or trailer to preventchafing.
6.7.6 Maintain lowest possible angle between floor and tie down cable or chain 45° or less.
6.7.7
CAUTION
DO NOT block or shore up beneath rails or axles. DO NOT route chains or cables over tops of rails or axles.
Holes in ends of rails shall not be used for tie downs.
6.7.8 Tow bar may be stored when space is limited by removing cotter pin and pulling the hinge pin.
6.7.9 Tires shall be inspected for proper inflation (Figure 4-6).
6.7.10 For shipment of containerized engines, see Chapter 4.
6.8 TRUCK SHIPMENT.
Trailer mounted engines shipped by flatbed shall be tied down and blocked (Figure 6-1, Figure 6-2 and Figure 6-3).
NOTE
Enclosed trucks WILL NOT be used for dolly or trailer mounted engines unless equipped with floor mountedbull rings and proper tie down equipment.
6.8.1 Wheel chocks of wood (4 x 4 inches or 4 x 6 inches) shall be placed fore and aft of each wheel. The chocks shall bechamfered and toenailed to the carrier deck using 30 dd nails to further secure the engine.
6.8.2 NOMINAL 2 x 4 inches or wider blocks, approximately 18 inches or longer shall be nailed with 20 dd nails to thetruck floor or deck one inch from the outside of each tire, nail a second block on top of these blocks. These blocks willrestrict side movement without damage to the side wall of tires.
6.8.3 Dolly mounted engines shall be tied down, and in addition shall be secured by blocking or bracing to prevent lateral orlongitudinal movement. Timbers 2 inches thick and 4 or 6 inches wide shall be nailed to the floor or deck with 20 dd nails ateach end and each side of box, skid or dolly and blocks shall be not less than 18 inches in length. A second block of samesize and length shall be nailed on top of the first blocks using the same type of nails.
6.8.4 Engines in metal or FRP containers shall be tied down using one or more of the following methods:
6.8.4.1 Attach tie downs across container skids at each end and each side or from container pad eyes to truck anchors.
6.8.4.2 Attach cables, chains or strapping across top of container (protect container and tie down by use of cardboard placedunder tie down).
6.8.4.3 Steel strapping used for securing containers shall be at least one and one-half inches wide for truck transports; twoinches for rail shipment. Strapping shall conform to specification QQ-S-781 type I, class A. Strapping will be padded whenrouted over sharp edge or around corners.
6.8.4.4 When additional anchoring facilities are required to adequately secure engine container to transports by strapping,use anchor plates NSN 5340-00-252-3014 and 5340-00-252-3015 with gimlet point round head screws.
6.8.4.5 Canned engines loaded within the confines of closed vans will be secured by 2 x 4 inch blocks or with other freightand at the discretion of the transportation officer.
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6.9 CERTIFICATION AND SEALS.
6.9.1 The agent or personnel responsible for securing the engine on the carrier shall sign the applicable copy of thegovernment bill of lading in the area marked Blocked and Braced by . Authorized personnel shall sign the transportationcopy in the area marked Blocking and Bracing inspected by .
6.9.2 All closed VAN type trucks shall be sealed when the following conditions apply:
6.9.2.1 Truck is fully loaded.
6.9.2.2 When exclusive use of vehicle is requested by shipper.
6.9.2.3 When requested by the carrier.
6.9.2.4 When shipment is tendered at truckload rates.
NOTE
Seal numbers shall be applied to appropriate shipping document so number can be transferred to government billof lading.
Figure 6-1. Side View of Trailer Mounted Engine Loaded for Open Truck Shipment
6-3
TO 00-85-20
Figure 6-2. Front View of Trailer Mounted Engine Loaded for Open Truck Shipment
Figure 6-3. Close-Up View of Tie Down at Engine Mount
6-4
TO 00-85-20
Figure 6-4. Trailer 55J9109 with KC-97 Power Package Installed, Right Rear Three-Quarter View
Figure 6-5. Trailer 55J9109 with KC-97 Power Package Installed, Left Front Three-Quarter View
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TO 00-85-20
Figure 6-6. Recommended Tiedown Position for Air Shipment
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Figure 6-7. Engine Containers Double Decked
Figure 6-8. Engine Tie Down for Flat Car on Truck Shipment
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TO 00-85-20
6.9.3 When shipping 3000E1 trailer piggyback on a 4000 trailer, follow procedures in Figure 6-9 with the followingexceptions:
6.9.3.1 Prepare the 4000 trailer by centering the lateral and rotational adjustments.
6.9.3.2 Lower rails until upper frame pads rest on lower frame pads.
6.9.3.3 Raise the 4000 trailer main frame to maximum height.
6.9.3.4 Open both relief valves to engage wheel cylinder locks. Return both relief valves to the closed position when thewheel cylinder lock has been engaged.
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TO 00-85-20
Figure 6-9. Shipment of Engine Transportation Trailers
6-9
TO 00-85-20
Figure 6-10. Shipment of Engine Transportation/Installation Trailers
6-10
TO 00-85-20
6.10 LOADING UNITED TRAILER FOR AIR TRANSPORT.
The trailer, with power plant, may be air transported in either a C-130, C-141A, or C-5 aircraft. The procedure to load thetrailer is the same for all aircraft. However, the trailer must be loaded into the C-130 and C-141A aft and first. Loading thetrailer into a C-5A, either end can go first. It is recommended that the trailer be winched aboard the aircraft and the aft and/orforward manual steering utilized as required. It is necessary to have observers inside and outside the aircraft to be certain allclearances are maintained. The following procedure is for use with C-130 and C-141A aircraft with notes to delineate theoptions for the C-5A. Read the entire procedure before starting. Proceed as follows:
6.10.1 With the towing vehicle, position the trailer directly in line with the aircraft loading ramp. It may be necessary tomaneuver the trailer by hand and manually steer it both fore and aft.
6.10.2
CAUTION
Remove the foot pads if they are installed in place and stow them on the top of the mainframe side rails asprovided. Failure to comply will prevent proper clearances to be maintained.
Attach a sling to the rear (front or rear for C-5A), tie down rings and connect the aircraft cargo winch to its center.
6.10.3 Position the observers, release the parking brakes and start the winch.
6.10.4 If necessary, make any minor steering adjustments that are required to maintain side clearance.
6.10.5
CAUTION
Always reinstall the locking cylinder pins after operating the hydraulic lift mechanism. Failure to comply couldresult in excess power plant shock should any failure occur in the hydraulic system.
Stop the winch when the ground clearance becomes inadequate.
NOTE
When the trailer is being winched aboard an aircraft, initially the ground clearance is critical and must bemaintained. At some point when one set of wheels are on the ramp and one set in the aircraft, the ceilingclearance becomes critical.
6.10.6 Operate the hydraulic lift mechanism and increase the floor/ceiling clearance as required, while observing theceiling/floor clearance to maintain adequate overall clearance. Replace the locking cylinder pins.
6.10.7 Start the winch.
6.10.8 Repeat paragraph 6.10.6, paragraph 6.10.7 and paragraph 6.10.8 as many times as necessary until all four trailerwheels are on the same plane.
6.10.9 Install the foot pads.
6.10.10 When the trailer and power plant have been winched to the position desired, set the aft parking brakes and fullykneel the trailer.
6.10.11 Set the forward parking brakes and close the hydraulic pump bleed valve and metering valve.
6.10.12 After the trailer is positioned on the carrier, secure it with chains or cables as shown in Figure 6-10.
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6.11 LOADING LOCKHEED ENGINE TRAILER IN AIRCRAFT, TF39.
NOTE
In case of conflict between these instructions and applicable aircraft loading instructions, the applicable aircraftloading instructions shall be followed.
6.11.1 Tow the trailer to the vicinity of the aircraft loading ramp. Unkneel the trailer.
6.11.2 Remove and stow foot pads from the front of the trailer.
6.11.3 Load and position trailer on the aircraft. The rear towbar may be used for manual steering.
6.11.4 Straighten front and rear wheels and install lock pin in rear tongue. Secure trailer by engaging front and rearhandbrakes.
6.11.5 Secure trailer in accordance with applicable loading instructions using tie-down rings.
6.12 LOADING ENGINE TRAILER ON FLAT BED TRUCK OR RAILWAY FLAT CAR, TF39.
WARNING
Carrier bed must be of sufficient width, or incorporate outriggers to provide full contact with trailer tire treads.No tread overhang shall be permitted.
6.12.1
CAUTION
• Hoist the trailer only at the four rings located on outside corners of main frame marked hoist ring.
• Due to engine height, and to prevent engine bearing damage, use only lowboy air suspension or railway airsuspension when transporting engine by surface transportation.
• The trailer must be in the unkneeled position. Shipping in the kneeled position could result in damage to thetrailer and/or engine.
The trailer, with an engine installed, may be loaded on the carrier with a tow vehicle which has facilities for air brakesystems.
6.12.2 The trailer/engine combination may be loaded on the carrier using a crane and sling. The sling must have spreaderbars to assure the four cables clear the engine.
6.12.3 After trailer is positioned on carrier, remove and stow front towbar in a convenient location on truck bed/flat car.Secure trailer by attaching tie-down chains or cables to the tie-down/hoist rings as shown in Figure 6-10.
6-12
TO 00-85-20
Figure 6-11. Position of Tiedown Chains or Cables
6-13
TO 00-85-20
6.13 TIEDOWN INSTRUCTIONS FOR MULTI-PURPOSE TRAILER, F108.
6.13.1 Load engine/trailer on flatbed in accordance with paragraph 5.14.
6.13.2
CAUTION
• Rear tiedown, for engines with QEC Kit installed, must be checked to ensure sufficient clearance existsbetween ring cowl and tiedown. Insufficient may result in costly engine damage.
• When preparing F108 engines for surface shipment, ensure no tiedowns cross over any position of the cradleand shock mount assembly. Any tiedown attached to or which passes over cradle and shock mount assemblywould eliminate shock damping features and result in engine bearing damage.
Attach and secure tiedowns to front, rear and sides of trailer in accordance with Figure 6-11, Figure 6-12, and Figure 6-13.
6.14 TIEDOWN INSTRUCTIONS FOR F108 ENGINE STAND (PART NUMBER 856A1200) (FIGURE 6-15 AND
FIGURE 6-16).
6.14.1 Load engine/stand on flatbed in accordance with paragraph 5.15.
6.14.2
CAUTION
• To ensure vibration dampening feature of the shipping stand is not nullified, there must be a minimumclearance of 1.5 inches (38 mm) between the lowest part of engine or shipping stand cradle and trailer bed. Ifnecessary, wood shoring can be placed beneath the stand base, forklift tunnels and trailer bed in order toachieve the required minimum clearance. Shoring must be placed beneath stand so that it does not protrudeinboard within the vertical plane movement of cradle.
• Tie-down chains and straps must be installed properly and attached solely to tie-down rings. Loose ends of tie-down must be kept clear from the top and underneath engine/stand. If improper tie-down is performed, thevibration dampening feature of the shipping stand shock mounts will be nullified resulting in possible enginebearing damage from excessive G loads.
Anchor the engine/stand base to the flatbed by tie-down straps or chains.
NOTE
There are ten tie-down rings on the stand base. Any combination can be used; however, use of the rings located atthe four inside corners of the stand base is recommended.
6.14.3 Attach tie-downs to rings and pull them diagonally along the truck bed to anchoring points on the flatbed. Pull all tie-down chains or straps taut and secure (Figure 6-15).
6.14.4 Acceptable alternate method is to pass chains or straps through the engine/stand base forklift tunnels. Pull tie-downsforward and aft along side of flatbed and secure to anchoring points. Pull all tie-down chains and straps taut and secure(Figure 6-16).
6-14
TO 00-85-20
6.15 F110 ENGINE SHIPPING AND STORAGE STAND GENERAL INFORMATION.
6.15.1 The ETU-114/E Engine Shipping and Storage Stand is intended for transportation and storage of the F110-GE-100Turbofan Engine with augmenter installed. The shipping and storage stand consists of an outer rigid supporting structure andan inner frame attached to the support structure by an elastic suspension. The inner frame includes provisions for supportingthe engine by the flight support points.
6.15.2 The physical size of the ETU-114/E Engine Shipping and Storage Stand is as follows:
(1) WITH ENGINE INSTALLED:
Length = 186 inches
Width = 48 inches
Height = 56 inches
Cube = 289.3 feet
Weight (maximum) = 5620 pounds
(2) EMPTY:
Length = 90 inches
Width = 48 inches
Height = 56 inches
Cube = 140.0 feet
Weight = 1020 pounds
6.15.3 Two-way forklift entry is provided to permit handling by forklift truck.
6.15.4 Four hoisting eyes provided on the top to permit hoisting with a four part sling.
6.15.5 Unloaded stands may be stacked two-high for transportation and storage. Loaded stands may be stacked two-high forstorage but not for transportation. Tapered guide pins are provided to aid stacking alignment. A positive stacking interlock islocated at each corner.
6.15.6 Four rings are provided along the top of the stand that may be used for surface transportation tie down. These may beused in various combinations to tie down a single stand or groups of two or more stands. In addition, there are two lowerloops that are used for air transport tiedown only.
6.16 ETU-114/E STAND SURFACE TRANSPORTATION, F110.
6.16.1 Surface transportation of engines, an air ride tractor and trailer will be used. The trailer must be at least 40 feet inlength.
NOTE
Nylon straps are the preferred method of tiedown.
6.16.2 Engine stand forward and aft movement will be restricted by the use of 2 inch x 6 inch x 24 inch blocks, nailed to thebed of the trailer with 2 odd nails at all four corners (Figure 6-17.)
6.16.3 Multiple shipment engine stands will be side by side, with the stand upright members parallel. The engines will faceone forward and one aft. The engines must be at least one foot from the forward or aft end of the trailer. The distancebetween two engines on the same side of the trailer must be at least two feet (Figure 6-14).
6.16.4 Four upper tiedown rings will be utilized for surface transportation. Do not use the lower loops (Figure 6-17).
6-15
TO 00-85-20
6.17 PLACEMENT FOR THE SHIPMENT OF 1, 2, 3 AND 4 ENGINES, F110.
6.17.1 One engine:. Placed on the center of the trailer.
6.17.2 Two engines:. Placed on the center of the trailer.
6.17.3 Three engines:. Two engines placed forward on the trailer and one engine placed on the rear of the trailer.
6.17.4 Four engines:. Two engines placed forward on the trailer and two engines placed on the rear of the trailer.
6-16
TO 00-85-20
Figure 6-12. Front Tiedown
6-17
TO 00-85-20
Figure 6-13. Rear Tiedown
6-18
TO 00-85-20
Figure 6-14. Side Tiedowns (2 sides)
6-19
TO 00-85-20
6.18 AIR TRANSPORTATION, F110 (FIGURE 6-20).
6.18.1 Air transportation of engines/stands will utilize the HCU-6/E pallet.
6.18.2 Four upper tiedown rings and two lower tiedown loops will be utilized for air transportation.
6.18.3
CAUTION
Use only a four-part sling with a minimum reach of 50 inches. Stands with engines installed may be stacked twohigh for storage purposes. Stands with engines will not be shipped stacked.
Single engine shipment, the engine will face forward. Dual engine shipment (paragraph 6.16.3).
NOTE
Use a four-part sling with a minimum reach of 50 inches.
6.18.4 Remove the four quick disconnect locking pins from the bottom stand.
6.18.5 Lift stand and lower onto the lower stand using the tapered locating pins as a guide.
6.18.6 Insert the four quick disconnect pins of the lower stand into the tapered locating pins protruding through the base ofthe upper stand.
6.19 UNSTACKING ETU-114/E STAND, F110.
6.19.1 Remove the four quick disconnect pins from the lower stand’s tapered locating pins.
6.19.2 Raise the upper stand from the lower stand.
6.19.3 Replace the quick disconnect locking pins in storage holes on the lower stand.
6-20
TO 00-85-20
Figure 6-15. Surface Transportation, F110
6-21
TO 00-85-20
Figure 6-16. F108 Transportation Stand Tie Down
6-22
TO 00-85-20
Figure 6-17. F108 Transportation Stand Tie-Down (Alternate Method)
6-23
TO 00-85-20
Figure 6-18. Nylon Strap Tiedown (Preferred Method)
6-24
TO 00-85-20
Figure 6-19. Chain Tiedown (Alternate Method)
6-25
TO 00-85-20
Figure 6-20. Stack Stand Tiedown
6-26
TO 00-85-20
Figure 6-21. HCU-6/E Pallet Tiedown
6-27
TO 00-85-20
6.20 LOADING TT90-F-503/TT90-F-505 TRAILER AND F117-PW-100 ON A FLAT BED TRAILER USING TOW
VEHICLE.
WARNING
The MB-2 tow vehicle is the only authorized tow vehicle for towing the lift trailer on flat surfaces and up to 15%slopes. The bobtail vehicle shall only be used for towing on flat surfaces and up to 3% slopes. When thesevehicles are not available, use Table 1 of this supplement to determine an equivalent vehicle. Failure to complycould cause injury to personnel or damage to equipment.
WARNING
• The MB-4 tow vehicle shall not be used for towing of the lift trailer until completion of TCTO 35D3-3-79-511 is complied with on that specific lift trailer due to the dynamic braking and hard stops of this vehicle.Failure to comply could cause injury to personnel or damage to equipment.
• Forklift type vehicles with clevis drop pin shall not be used for towing of the lift trailer. Failure to complycould cause injury to personnel or damage to equipment.
CAUTION
• The Engine Transport trailer assembly requires a special drive on “Low Boy” tractor trailer with removalgoose neck adaptor which allows the air ride flatbed to be lowered within inches of the ground for loading.
• Loading of the TT90-F transportation trailer with engine installed shall not be accomplished using a forkliftbecause the forks will damage the engine.
• Carrier’s tractor-trailer bed must have a sufficient width to accommodate the wheelbase of the engine trailer.Tire tread hang over is not permitted.
• The tow vehicle must be equipment with a pintle hook and have a minimum drawbar rating of the grades/ramps with conditions reduce traction. See Figure 1 table “Towing Force Calculation”.
NOTE
SEE T.O. 35D3-3-3-80-1, TABLE 1 - TOWING FORCE CALCULATIONS FOR ENGINE TRAILERTOWING VEHICLE.
6.20.1 Using a tow vehicle equipped with a pintle hook, position the Trailer with the centerline of the tractor trailer ramp.Disconnect trailer brake system (quick disconnect) coupling to aid in backing.
6.20.2 Set engine trailer’s forward and aft hand brakes.
6.20.3 Install steering bar at engine trailer’s rear (engine fwd) steering assembly. Remove pin from the steering linkage arm.
6.20.4 Release engine trailer’s front and rear brakes.
6.20.5 Push back the engine trailer up the flat bed ramp, making minor steering adjustments with the steering bar.
6.20.6 Set the forward hand brakes only. Reconnect brake hose coupling.
6.20.7 Disengage tow vehicle. Stow engine trailer draw bar in the vertical position and install lock pin.
6.20.8 Remove and stow the trailer steering bar. Install lock pin in the trailer rear steering linkage arm.
6.20.9 TT90-F-503 with articulating pins.
6-28 Change 2
TO 00-85-20
6.20.9.1 Remove lift mechanism articulating pins. Actuation of the hydraulic hand pump may be required to easily removearticulating pins.
6.20.10 TT90-F-505.
WARNING
Do not attempt to lower the trailer after actuator locking blocks have seated against the hydraulic actuator.Failure to comply may result in injury to personnel or damage to trailer.
6.20.10.1 Shoring dimensions shall be as follows: four stacks 20 inches L X 11 inches W X 14 to 16 inches H. Each stackof shoring shall be placed under the trailer and frame, centered under the SHORING markings. To prevent shifting duringtransport, the shoring stack-up should be fastened together using glue, nails, straps or screws. Additional shim pieces may berequired to ensure even contact between the shoring and the frame after the trailer is lowered.
6.20.11 TT90-F-503.
6.20.11.1 Operate the hand pump and lower the engine trailer onto the tractor-trailer flatbed surface. Making sure the traileris evenly lowered to prevent tipping.
6.20.11.2 TT90-F-505.
Railer trailer frame to clear lumber shoring using the trailer’s hand pump and selector valves. Place the shoring under thetrailer frame as shown in Figure 6-22A.
6.20.11.3 TT90-F-505.
Operate the hand pump and appropriate selector valves to lower trailer until the frame rests firmly on the shoring in all fourlocations.
6.20.12
CAUTION
Do not attach cables, chains, or strapping across the top of the engine, shipping cradle, or trailer rails. If impropertie down is performed, the shock and vibration damping feature of the engine trailer is nullified, resulting inserious damage to the engine during shipment.
Check that all four hand brakes are set. Chocking of the wheel is recommended per paragraph 6.8.
6.20.13 Secure with chains and binder that comply with D.O.T. 393-102 standards. Use a cargo strap to secure drawbar totruck trailer to prevent lateral movement. Optional: The drawbar can be removed and secured on the trailer bed.
6.20.14 TT90-F-503.
6.20.14.1 Install tarpaulins cover over engine and secure with 2x3 boards nailed together and secure to the bed of thecarriers trailer to prevent vibration and flapping damage during transport.
6.20.15 TT90-F-505.
6.20.15.1 Ensure the engine is sealed in a shipping bag or plastic sheeting per paragraph 4.4. Install tarpaulins over engineand secure using elastic bungee cords, rubber straps, etc. Do not allow metal hardware to come in contact with the engine toprevent impact damage during transport.
6.20.16 Comment:
a. Release rear brake (-503 and 505). Add steps to raise the -503 trailer from the floor of the flat bed trailer and installarticulating pins.
Change 2 6-29
TO 00-85-20
b. Add step to raise the -505 to remove shoring from under frame. Add step to lower the -505 trailer until actuatorlocking blocks have seated against the Hydraulic actuator.
c. Lower front draw bar (-503 and 505)
d. Install rear steering bar (-503 and 505)
e. Connect tow vehicle to draw bar (-503 and 505)
f. Release front brakes (-503 and 505)
g. Tow trailer from truck trailer (-503 and 505)
(Do not disconnect brake line to pull trailer off of truck, brake system is needed to slow trailer down as it is pulleddown the ramp.) (-503 and 505)
6.21 LOADING TT90-F TRAILER IN AIRCRAFT, F117-PW-100.
6.21.1 The trailer with the power plant may be transported in either the C-17 or C-5 transport Aircraft. It is recommendedthat the trailer be winched aboard the aircraft aft engine first using the trailer aft steering assembly to maintain clearance. Theuse of observers both inside and outside are required to insure clearances are maintained.
NOTE
Aircraft Loading Instructions, if available, shall override the instructions below.
6.21.2 With tow vehicle, position the trailer in line with the aircraft loading ramp. Manual movement may be required forproper alignment.
6.21.3 Set trailer’s front and rear brakes. Disengage tow vehicle.
6.21.4 Remove trailer towbar (aft engine) and stow.
6.21.5 Install steering bar at trailer rear (engine front) steering assembly. Remove pin from the aft steering stabilizing rod.
6.21.6 Attach a sling to the trailer front tiedown rings and connect the cargo winch to the sling.
6.21.7
CAUTION
Ground clearance is critical when loading into aircraft cargo areas. Clearance is most critical when the trailerwheels crest the loading ramp onto the cargo floor and the trailer remaining wheels are still on the loading rampresulting in reduced ceiling clearance.
Release trailer front and rear brakes.
6.21.8 Start winch and make minor steering adjustments as required using the trailer’s rear steering bar.
6.21.9 Stop winch once the desired position has been obtained.
6-30 Change 2
TO 00-85-20
Figure 6-22. Transportation Trailer Tiedown Configuration (Flatbed Truck)
6.21.10 Set trailer’s rear brakes (engine front).
6.21.11 Remove lift mechanism articulating pins. Actuation of the hydraulic lift mechanism may be required to easilyremove articulating pins.
6.21.12 Operating the hydraulic lift mechanism, lower the trailer onto the cargo floor.
6.21.13
CAUTION
Do not attach cables, chains, or strapping across the top of the engine or isolated cradle assembly of this shippingsystem.
Remove and stow rear steering bar.
6.21.14 Remove winch and secure with chains or cables as Figure 6-23 (Sheets 1 and 2).
Change 2 6-31
TO 00-85-20
Figure 6-23. Transportation Trailer Tiedown Configuration (Sheet 1 of 2)
6-32
TO 00-85-20
Figure 6-23. Transportation Trailer Tiedown Configuration (Sheet 2)
6-33
TO 00-85-20
6.22 LOADING 150504-1 INSTRUCTIONS FOR SURFACE TRANSPORTATION, F117-PW-100.
6.22.1 The Engine Transport trailer assembly requires a special “Low Boy” tractor trailer with removable goose neckadaptor which allows the air ride flatbed to be lowered within inches of the ground for loading.
6.22.2 If shipping only one engine on the tractor trailer, the aft end of the engine should be placed on the forward part of thetrailer near the gooseneck. No additional freight shall be permitted.
6.22.3 If two engines are shipped on a single stepped truck trailer, the engines should be placed such that the forward endsof the engine face each other at the center of the truck trailer. Ensure sufficient separation to avoid contact with the otherengine.
6.22.4 Forklifts used to handle engines in shipping stands or transportation trailers must have a lifting capacity equal to orgreater than the gross weight of the engine and shipping stand.
6.22.5 The following steps cover the loading and tie-down of the engine using the PW Transportation Stand (P/N 150504-1). This stand is normally used for transportation between the manufacturer and the airframer.
NOTE
Forklifts used to handle engines in shipping stands must have a lifting capacity equal to or greater than the grossweight of the engine and shipping stand. The outer end of the forklift prongs should be long enough to fully catchthe support rail on the opposite side of the stand.
6.22.5.1 Using appropriate forklift, enter the shipping stand support lift rails from the sides only. Secure a safety chainbetween the Transportation Stand base and the forklift.
CAUTION
Do not attach cables, chains, or strapping across the top of the engine or across the engine cradle section of theshipping system. Improper tie-down can lead to external hardware damage and bearing damage by nullifying theshock damping features.
6.22.5.2 Load and position engine/Transportation Stand on the trailer.
NOTE
Position tie-down chains or cables to avoid contact with each other, parts of the engine, or trailer to preventchafing.
6.22.5.3 Secure engine/Transportation Stand by attaching tie-downs per Figure 6-23 and pull all tie-down chains and strapstaut.
6.22.5.4 Install tarpaulins and secure with 2x3 boards nailed into the bed of the trailer to prevent vibration and flappingduring movement.
6-34 Change 2
TO 00-85-20
Figure 6-24. Truck Trailer Tie-Down
6-35
TO 00-85-20
Table 6-1. Trailer
ENGINE/GROSS/GROSSENGINE TYPE ADAPTER/WEIGHT TYPE TRAILER/WEIGHT WEIGHTF117-PW-100 1730012509737/2700# 1740012538064/11700# 11500#/25900#
Table 6-2. Trailer
ENGINE DEVICE GROSSENGINE NSN P/N DIMENSIONS WEIGHT WEIGHT WEIGHTF117 Inlet Fan 8145013883770 P60019 67 x 67 x 61 510# 772# 1282#
F117 Core 8145013886660 P60022 8x3 x 77 x 56 920# 2210# 3130#
F117 HPT 8145013883770 P60018 67 x 67 x 61 720# 577# 1297#
F117 LPT 8145013883792 P60023 67 x 67 x 61 1115# 787# 1902#
F117 Main 8145013883019 P60021 57 x 39 x 42 170# 690# 860#Gearbox
F117 Angle 8145013883021 P60020 38 x 36 x 29 63# 305# 368#Gearbox
F117 Trailer 1740012538064 TT90-F 331 x 96 x 57 11500# 11700# 25900#
F117 Cradle 1740012509737 17G230005-1 136 x 96 x 61 11500# 2700# 25900#Adapter
Table 6-3. Shipping Device Weights
ENGINE CONTAINER STOCK NUMBERF117-PW-100 P60018 Fiberglass 8145013883770
F117-PW-100 P60019 Fiberglass 8145013885805
F117-PW-100 P60020 Fiberglass 8145013883021
F117-PW-100 P60021 Fiberglass 8145013883019
F117-PW-100 P60022 Fiberglass 8145013886660
F117-PW-100 P60023 Fiberglass 8145013883792
6.23 F118-GE-101 ENGINE TIE DOWN INSTRUCTIONS FOR TRAILER (PART NUMBER 75GH109).
6.23.1 Surface transportation of the F118-GE-101 engine requires the use of Air Ride Tractor and Trailer.
NOTE
No additional freight authorized when shipping an F118-101 Engine. A exclusive/dedicated tractor-trailer mustbe used.
6.23.2 If shipping only one engine on the tractor-trailer, the aft part of the engine should be placed on the forward part ofthe trailer near the gooseneck.
6.23.3 If two engines are shipped on a single tractor-trailer, the engines should be placed such that the forward ends of theengine face each other at the center of the truck trailer. Ensure sufficient separation to avoid contact with the other engine.
6-36 Change 6
TO 00-85-20
6.23.4
CAUTION
• Cables, chains, tarpaulins, or tie down devices shall not be thrown over the engine. Failure to comply mayresult in damage to engine and/or engine shipping bag.
• Failure to use the chaining configuration shown may result in the engine becoming disengaged from theshipping adapters and dropping between the trailer rails.
Secure engine/transportation trailer to Air Ride Tractor trailer as follows (Figure 6-24):
CAUTION
Failure to install spreader bars may result in the engine coming loose and falling during shipment.
6.23.4.1 Ensure spreader bars (2 each) are installed across trailer rails, one forward and one aft of the engine.
6.23.4.2 Ensure engine trailer is centered on flat bed tractor-trailer, equal distance from side to side.
6.23.4.3 Attach chain to forward most eyelet/hole on left front adapter. Route chain forward of adapter and under trailer railto right side of flat bed trailer, approximately 4 to 7 feet forward of engine (Detail A).
6.23.4.4 Attach chain to forward most eyelet/hole on right front adapter. Route chain forward of adapter and under trailerrail to left side of flat bed trailer, approximately 4 to 7 feet forward of engine (Detail A).
6.23.4.5 Attach chain to rear most eyelet/hole on right rear adapter. Route chain to right side of flat bed trailerapproximately 6 to 9 feet aft of engine (Detail B).
6.23.4.6 Attach chain to rear most eyelet/hole on left rear adapter. Route chain to left side of flat bed trailer approximately 6to 9 feet aft of engine (Detail B).
6.23.4.7 Attach chain to rear most eyelet/hole of left front adapter. Route chain to left side of flat bed trailer approximately6 to 9 feet forward of engine (Detail A).
6.23.4.8 Attach chain to rear most eyelet/hole of right front adapter. Route chain to right side of flat bed trailerapproximately 6 to 9 feet forward of engine (Detail A).
6.23.4.9 All chains will be tightened with equal tension in the same order as they were installed.
6-37
TO 00-85-20
Figure 6-25. F118-GE-101 Engine Tie Down Procedure
6-38
TO 00-85-20
6.24 LOADING AND TRANSPORTATION FOR F119 ENGINE.
6.25 PURPOSE.
This procedure will provide the information and instructions for loading and securing the F119 engine in preparation forsurface and air transportation.
6.26 GENERAL INFORMATION.
NOTE
• Engine shipments shall use the F119 Engine Shipping System (ESS) (P/N P4330450) and the 3000Etransportation trailer (3000E) (NSN 4800-000-00) or equivalent 10000 lb capacity transportation trailer. The3000E transportation trailer must use tire size 7.50 x 10, 10 ply rating, inflated to 90-100 PSI.
• The engine inlet must be mounted towards trailer towbar, but the trailer may face fore or aft with respect tothe transport truck bed.
6.27 INSPECTION OF 3000E TRANSPORTATION TRAILER.
NOTE
• Prior to mounting and packaging the engine/ESS on the 3000E, a thorough inspection of the 3000E must beperformed.
• Anomalies discovered in this inspection must be repaired prior to mounting or packaging the engine on that3000E trailer per technical orders which govern the inspection, repair, and part content of the trailers.
6.28 POSITIONING OF F119/ESS ON 3000E TRANSPORTATION TRAILER.
6.28.1 Mount F119/ESS on 3000E with engine inlet towards towbar.
6.28.2 Position F119/ESS on 3000E such that center of gravity symbol is located midway between the 3000E axles.
ENGINE DIMENSIONS ENGINE DEVICE GROSS(L x W x H) WEIGHT WEIGHT WEIGHT
F119 196 x 71 x 99 5000 lbs. 1450 lbs. 7550 lbs.
See Figure 6-25 through Figure 6-34
Weight is indicated in pounds. Dimensions are in inches and do not include towbar.
6.28.3 Tighten rail clamps on ESS roller adapters to 375-400 in-lbs. (See Figure 6-30).
6.29 F119 ENGINE SHIPPING INSTRUCTIONS.
WARNING
Proper material handling equipment must be used during ON and OFF loading operations to prevent injury topersonnel and damage to the engine.
NOTE
A loading ramp or bridge or lift platform is the preferred method to roll transfer an engine into a transportingvehicle.
6-39
TO 00-85-20
6.29.1 F119 Engine Ground Transport Shipping Instructions. .
NOTE
• Highway transportation of a properly secured F119 engine can be accomplished using either an air ridesuspension tractor/trailer or a conventional spring ride suspension tractor/trailer.
• Enclosed trailers are the preferred trailer type for transporting engines but may only be used if properlyequipped with sufficient floor mounted tiedown rings and proper tiedown equipment.
6.29.2 Loading F119/ESS/3000E Engine On Ground Transport Vehicle.
6.29.3 Roll On Loading (Preferred Method).
WARNING
Proper material handling equipment must be used during ON and OFF loading operations to prevent injury topersonnel and damage to the engine.
CAUTION
There must be sufficient personnel on hand to safely handle the combined weight of the F119, ESS, and 3000E,particularly if the transporting vehicle has an inclined cargo bed.
NOTE
If a forklift or tug is unavailable, manually push the F119/ESS/3000E over the loading ramp onto the lift platformor onto the transporting vehicle.
6.29.3.1 Use a forklift or other suitable tug to push the F119/ESS/3000E onto the lift platform or onto the transportingvehicle.
6.29.3.2 Position 3000E parallel with truck bed, centered laterally.
6.29.3.3 Engage both 3000E wheel brakes.
6.29.4 Lift On Loading (Permitted Only If Loading Ramp Is Unavailable).
CAUTION
The forklift must have sufficient lift capacity, lift range, reach and time length to safely support, raise andposition the F119/ESS/3000E on the transporter vehicle. See weight summary in Section 2.0 GeneralInformation.
NOTE
This procedure is applicable only to flatbed or softside enclosed vans.
6.29.4.1 Align the F119/ESS/3000E close to and parallel with the truck bed.
6.29.4.2 Set both wheel brakes on 3000E.
6.29.4.3 Remove towbar from steering mechanism on 3000E.
6.29.4.4 Position the tines of the forklift truck under the rails of the 3000E as shown in Figure 6-28.
6-40
TO 00-85-20
CAUTION
Movement of the forklift must be minimized any time the F119/ESS/3000E is supported on the forklift tines.
6.29.4.5 Lift the F119/ESS/3000E straight up with clearance sufficient to clear the truck bed.
6.29.4.6 Carefully center the F119/ESS/3000E on the truck bed.
6.29.4.7 Lower the F119/ESS/3000E onto the flatbed transporter.
6.29.4.8 Reinstall towbar to steering mechanism of trailer.
6.29.5 Hoist On Loading Is Not Permitted.
6.29.5.1 Ensure that F119/ESS/3000E is positioned parallel with truck bed, laterally centered.
6.29.5.2 Ensure that both 3000E wheel brakes are fully engaged.
6.29.5.3 Place chamfered wooden wheel chocks (4x4 inches) fore and aft of each 3000E wheel. Toenail the chocks to thetruck bed using 30 dd nails as shown in Figure 6-31. These blocks will restrict side movement without damage to the tire sidewall.
6.29.5.4 Nail blocks 2x4x18 inches minimum to the truck bed using 20 dd nails one inch from the outer sidewall of eachtire. Nail a second block on top of the first as shown in Figure 6-31. These blocks will restrict side movement withoutdamage to the tire side wall.
6.29.5.5 Secure trailer towbar using 20 dd nails as shown on Figure 6-30.
WARNING
Tiedown chains must be 10000 lb capacity minimum and be attached per tiedown geometry on Figure 6-25,Figure 6-26 and Figure 6-27.
6.29.5.6 Attach tiedown chains or cables to ESS tiedown rings and to truck bed as shown in Figure 6-25 throughFigure 6-27.
NOTE
Holes in end of trailer rails are not to be used for attaching tiedown chains or cables.
6.29.5.7 Tighten tiedown chains or cables incrementally with roughly equal tensions so that transportation trailer cannotmove.
6.29.5.8 Cover F119/ESS/3000E with 20 foot x 40 foot tarp and secure to truckbed using tiedown straps.
6.29.6 F119 Engine Air Transport Shipping Instructions (For ESS/3000E Trailer Mounted Engines Only).
NOTE
The F119 engine may be air transported on C130, C141, C5, and C17 transport aircraft provided the aircraft arefitted with appropriate floor tiedown receptacles.
6-41
TO 00-85-20
6.29.7 Loading F119 Engine on Transport Aircraft.
6.29.8 Roll On Loading (Only Approved Method).
CAUTION
The packaged F119/ESS/3000E must be pulled into the transporting aircraft engine inlet first. Failure to observethis caution may result in damage to the engine exhaust nozzle tip.
.
NOTE
The aircraft loadmaster shall supervise all aspects of loading, positioning, and securing the packagedF119/ESS/3000E into the transport aircraft.
6.29.8.1 Pull the packaged F119/ESS/3000E into the transport aircraft by attaching the internal aircraft winch to the towbarof the 3000E trailer.
6.29.8.2 Position 3000E parallel with aircraft cargo bed, laterally centered, symmetrical with 10000 lb capacity floortiedown receptacles.
6.29.8.3 Engage both 3000E wheel brakes.
6.29.9 Lift On Loading Is Not Permitted. .
6.29.10 Hoist On Loading Is Not Permitted.
6.29.11 Securing F119 Engine in Transport Aircraft.
6.29.11.1 Ensure that F110/ESS/3000E is positioned parallel with aircraft cargo bed, laterally centered, symmetrical with10000 lb capacity floor tiedown receptacles.
6.29.11.2 Ensure that both 3000E wheel brakes are fully engaged.
WARNING
Tiedown chains must be 10000 lb capacity minimum and be attached per tiedown geometry on Figure 6-34.
6.29.11.3 Attach tiedown chains or cables to ESS tiedown rings and to aircraft cargo bed as shown in Figure 6-32.
NOTE
Holes in end of trailer rails are not to be used for attaching tiedown chains or cables.
6.29.11.4 Tighten tiedown chains or cables incrementally with roughly equal tensions so that transportation trailer cannotmove.
6-42
TO 00-85-20
Figure 6-26. F119/ESS/3000E Overall Dimensions and Truck Tiedown Configuration - Front View
6-43
TO 00-85-20
Figure 6-27. F119/ESS/3000E Overall Dimensions and Truck Tiedown Configuration - Side View
6-44
TO 00-85-20
Figure 6-28. F119/ESS/3000E Overall Dimensions and Truck Tiedown Configuration - Plan View
6-45
TO 00-85-20
Figure 6-29. Positioning of Heavy Duty Forklift Tines for Lifting F119/ESS/3000E onto a Flatbed Truck
6-46
TO 00-85-20
Figure 6-30. Tighten Rail Clamps to 375-400 IN LBF
6-47
TO 00-85-20
Figure 6-31. Block and Secure Towbar to Truckbed
6-48
TO 00-85-20
Figure 6-32. Block and Chock 3000E Trailer Tires On Truck Bed
6-49
TO 00-85-20
Figure 6-33. F119/ESS/3000E Overall Dimensions and Cargo Aircraft Tiedown Configuration - Front View
6-50
TO 00-85-20
Figure 6-34. F119/ESS/3000E Overall Dimensions and Cargo Aircraft Tiedown Configuration - Side View
6-51
TO 00-85-20
Figure 6-35. F119/ESS/3000E Overall Dimensions and Cargo Aircraft Tiedown Configuration - Plan View
6-52
T.O. 00-85-20
CHAPTER 7ENGINE SHIPPING DEVICE MANAGEMENT
7.1 The Comprehensive Engine Management System (CEMS) will provide the Base Engine Manager with a means ofmaintaining the on-hand quantity and serviceability of non-EMO engine shipping devices by type. This capability will beprovided by the automatic decrementing and incrementing of a counter each time an AF FORM 1534, which contains engineshipping device information in block 13, is entered into a 4 character alpha numeric code. These four codes, when combined,will provide exact information as to what type of trailer was used, if it was serviceable, and what type of adapter wasinstalled. Guidelines on the use of this expanded feature is outlined below.
a. Type Engine Shipping Device. The first position of this four character alpha numeric code will be used to identifythe type of engine shipping device used, i.e., container, trailer, stand, dolly, box, or pallet and its serviceability, ifapplicable. For example, this first column identifier (table 7-1) would use a “T” to indicate the item is a serviceabletrailer or an “F” to indicate it is a serviceable full container, etc.
b. Engine Trailers. The second and third column identifier, when used in conjunction with the first column identifier fortrailers, serves to provide more specific information about the trailer. The second and third column identifiers (table7-2) correspond to a specific engine trailer stock number. For example, “AL” is the code assigned to engine trailerNSN 1740-00-516-7930.
c. Engine Shipping Containers. When the first column identifier indicates the item is an engine container, the second,third and fourth column identifiers are combined to specify exactly which container (table 7-4), by NSN, is beingused. For example, code “ABT” represents NSN 8145-00-285-6110. This code, when combined with a first columnidentifier (table 7-1) for containers such as “J”, would indicate the stock number of the container plus indicate that itwas a non-serviceable half container.
d. Adapters. The fourth column identifier is used to identify the type of adapter on the engine trailer identified by thesecond and third column identifiers. For example, if adapter NSN 1730-00-589-9465 were used, its code would be“N” (table 7-3).
e. Other Codes. In addition to providing codes for trailers, containers and adapters, a single character code is providedfor stands, dollies, boxes and pallets (table 7-1). This single code serves as the first column identifier while thesecond, third and fourth column identifiers remain blank. Also, to preclude duplicate counting of containers, pallets,etc., when more than one engine/module is shipped in the same container a “9” code is used. This code is inserted inblock 13 of the AF FORM 1534 for the second, third, etc., engine/module shipped in the same container and fills allfour column identifiers (i.e., 9999).
NOTE
Until CEMS is implemented, only the first position code (table 7-1) will be repeated on the AF FORM 1534.
f. Identification and Marking. All engine shipping devices, containers, adapters, and trailers will be marked with theproper NSN using the following methods.
(1) If the manufacturers data plate contains a valid and legible NSN, no further marking is required for that item.
(2) For trailers, metal containers, and fiberglass containers, use a paper stencil of the NSN (1/2” letters) and spraypaint the NSN on the device in a conspicuous plate.
(3) For adapters, select a smooth surface that will always be visible and vibropeen the NSN on the adapter.
(4) All base engine managers are responsible for ensuring that the devices at their stations be properly identified.
Change 1 7-1
T.O. 00-85-20
Table 7-1. Engine Shipping Devices - First Column Identifier Codes
NOUN CODE DESCRIPTIONTRAILER T Serviceable Trailer
TRAILER U Nonserviceable
CONTAINER F Full Container Serviceable
CONTAINER G Full Container Nonserviceable
CONTAINER H Half Container Serviceable
CONTAINER J Half Container Nonserviceable
STAND/DOLLY S -
BOX B -
PALLET P -
NOTE
These codes are not used to account for the shipment of empty engine devices (trailer, containers, adapters, boxes,etc.). These must be deleted or added to Shipping Device Status (SDS) system by the housekeeping TRIC EngineStatus Update (ESU) since no AF FORM 1534 will be involved.
Table 7-2. Engine Shipping Devices - Trailers - Second and Third Column Identifier Codes
CODE NSN P/N TMSAA 1740-00-294-3638 340552 T56
AB 1740-00-106-8512 200-000-101 T56
AC 1740-00-718-1579 404190-1 T56
AD 1740-00-488-9469 U533747 TF39
AE 1740-00-602-6365 4S30031-101A TF39
AF 1740-00-711-3135 60-H7553 J69
AG 1740-00-690-5284 107238 J60, T58
AH 1740-00-580-0494 MILT 26232 Multi-engine
AJ 1740-00-554-1667 104624 Multi-engine
AK 1740-00-534-0595 101671 Multi-engine
AL 1730-00-516-7930 100315 Multi-engine
AM 1730-00-655-7736 100315-500 Multi-engine
AN 1740-00-516-7929 100334 Multi-engine
AP 1740-00-713-5908 107640 Multi-engine
AQ 1740-00-713-5908 107640 TF33
AR 1740-00-051-3535 PDG0324 J60, J85
AS 1740-00-058-4955XD 11020MEC J60
AT 1740-00-713-5908 107640 T64
AU 1740-01-127-4954 STC90856-1 F108
AV 1740-00-554-1667 104624 F100-GE102
AW 1740-00-713-5908 107640 F100-PW-100/200/220/220/229
7-2 Change 1
T.O. 00-85-20
Table 7-3. Engine Shipping Devices - Adapters - Fourth Column Identifier Codes
CODE NSN P/NA 1730-00-036-7271 PDG4352
B 1730-00-051-3536 PDG0325
C 1730-00-051-3539 PDG0328E
D 1730-00-052-4450 PDA2675
E 1720-00-238-8019 68E25591-1
F 1730-00-485-8615 F71401
G 1730-00-573-5113 105064
H 1730-00-573-5114 105065
J 1730-00-573-5115 105067
K 1730-00-573-5116 105069
L 1730-00-574-2109 105003
M 1730-00-589-9464 105001
N 1730-00-589-9465 105004
P 1730-00-626-5691 105901
Q 1730-00-654-8388 106355
R 1730-00-657-1178 105865
T 1730-00-676-6848 8-96398-1
U 1730-00-676-6850 8-96398-5
V 1730-00-875-5399 F71401-2
W 1740-00-103-0870 P41640
X 1740-00-522-2754 101164
Y 1740-00-523-3572 PDG4543
Z 1740-00-734-6470 60D7559-3-5
1 1740-00-911-1026 P33003
2 4920-00-591-6975 21C5270G01
3 1730-00-238-8019 68E2559-1
4 1730-00-708-7948CN 6865331
5 1730-00-503-7625 P4006409
6 Other/Wrong Adapter
7 No Adapter Installed
8 1730-00-764-2441 21C2206G003
9 1740-00-059-7339 65700-70016-045
10 1740-01-189-4164 3C3461-G02
Change 1 7-3
T.O. 00-85-20
Table 7-4. Engine Shipping Devices - Containers - Second, Third and Fourth Position Codes
CODE NSN ENGINE TMSAAA 8115-00-526-2868 T56
AAB 8145-00-005-8744 J85-17/17A
AAC 8145-00-032-6705 J85-21
AAD 8145-00-044-8858 J85-T/13
AAE 8145-00-049-5204 T58-A7-A9
AAF 8145-00-200-2411 R2800
AAH 8145-00-292-9642 J69-T25
AAJ 8145-00-390-5561 R2800
AAK 8145-00-390-5563 R1830/R2000
AAL 8145-00-390-5565 R1300/R1820
AAM 8145-00-390-5574 J65
AAN 8145-00-399-6066 R3350-93/93A
AAP 8145-00-451-5228 T56-A15
AAQ 8145-00-465-6373 T400-GB400
AAR 8145-00-465-6374 T400-CP400
AAS 8145-00-550-7451 T56-A7-A9-A15
AAT 8145-00-614-4805 T53-L11A
AAU 8145-00-661-2972 G56-A7-A9-A15
AAV 8145-00-663-9802 T56-A7-A9
AAW 8145-00-687-8110 T56-A7-A9
AAX 8145-00-839-8418 T56-A7, A9-A15
AAY 8145-00-845-7668 J60
AAZ 8145-00-845-7670 J85-5/7/13
ABA 8145-00-111-5843PL T64
ABB 8145-00-871-8557 O-300,IO-360D,O-470-11B,G50-480-540
ABC 8145-00-887-1949 G56-A7-A9-A15
ABD 8145-00-888-3698 T56-A7-A9-A15
ABF 8145-00-927-1744 R1820/R2000
ABG 8145-00-929-9454 J85-5/13
ABH 8145-00-988-3676 J85-21/13
ABJ 8145-00-994-3822 J85-7
ABK 8145-00-994-3823 J85-5/13
ABM 8145-00-031-1497 J47-25/25A/27
ABN 8145-00-111-5843 T64-7/7A
ABP 8145-00-113-8946 T64-7/7A
ABQ 8145-00-113-8947 T64-7/7A
ABR 8145-00-193-8877 TF41-2/400
ABT 8145-00-285-6110 J47-25/25A/27
ABU 8145-00-290-1386 J79-2/3/7/11/15/15A
ABV 8145-00-390-5568 J33-35/35A
ABW 8145-00-390-5573 J33-35/35A
ABY 8145-00-390-5581 J33-35/35A
7-4 Change 1
T.O. 00-85-20
Table 7-4. Engine Shipping Devices - Containers - Second, Third and Fourth Position Codes - Continued
CODE NSN ENGINE TMSACB 8145-00-391-0487 J47-25/25A/27
ACC 8145-00-439-2463 TF41-2/400
ACD 8145-00-550-6205 J79-2/3/7/11/15/15A/17/17A/17C
ACE 8145-00-587-2431 J57-13/19/21/23
ACF 8145-00-590-4854 J79-2/3/7/11/15/15A/17
ACG 8145-00-597-5771 J47-25/25A/27
ACJ 8145-00-664-9558 J75-17/19/19W
ACK 8145-00-785-4807 J79-2/3/7/11/15/15A/17/17A
ACL 8145–00-785-4808 J79-2
ACM 8145-00-785-4809 J79-2/7/11/15/15A/17/17A/17C
ACP 8145-00-785-4811 J79-2/7/11/15/15Z/17/17A/17C
ACQ 8145-00-844-0050 TF33-3/11A
ACR 8145-00-855-0549 T58-3
ACS 8145-00-887-9328 J79-2/3/7/11/15/15A/17/17A/17C
ACT 8145-00-901-6327 T64-7/7A
ACW 8145-00-928-4859 T58-5
ACY 8145-00-988-3674 T58-3
ACZ 8145-00-988-3679 T58-3
ADA 8145-00-901-6327 T64
ADB 8115-00-901-6327 T64
ADC 8115-NL GTCP8570//85180/85397/T62
ADD 8145-00-390-5572PJ J33
ADG 8145-00-394-6561PT (Metal) F100-23C/24C Fan Drive
8145-01-116-9590PT
ADH 8145-00-394-6566PT (Metal) F100-23A/24A Inlet Drive
8145-01-116-9588PT
ADJ 8145-00-394-6673PT (Metal) F100-23G/24G Gearbox
8145-01-116-9586PT
ADK 8145-00-390-5575 R4360-59B63A
ADM 8145-00-251-9495 J85-17/17A
ADN 8145-00-901-6427 T64
ADQ 8145-00-394-6562PT (Metal) F100-23F-24F Augmentor
ADS 8145-00-772-7866 T53
ADT 8145-01-116-9586PT (Fiberglass) F100-23G/24G Gearbox
ADU 8145-01-116-9587PT (Fiberglass) F100-23B/24B Core
ADV 8145-01-116-9588PT (Fiberglass) F100-23A/24A Inlet Drive
ADW 8145-01-116-9589PT (Fiberglass) F100-23F/24F Augmentor
ADX 8145-01-116-9590PT (Fiberglass) F100-23C/24C Fan Drive
ADY 8145-01-035-1387PT (Metal) F100-23H/24H HPT
ADZ 8145-00-396-2056PT (Metal) F100-23B/24B Core
AEA 8145-00-394-6566PT F100-24A
AEB 5305-00-558-5047 J79
AEC 8145-00-785-4810AN J79
AED 8145-00-292-9642AS J69
Change 1 7-5
T.O. 00-85-20
Table 7-4. Engine Shipping Devices - Containers - Second, Third and Fourth Position Codes - Continued
CODE NSN ENGINE TMSAEE 8145-00-813-4558 J60
AEF 8145-00-048-7394RU J57
AEG 8145-00-626-3681AN J57/J75
AEH 8145-00-674-7656AN J57/J75
AEJ 8145-00-405-3279PQ TF30
AEK 8145-00-070-3684AN J79
AEL 8145-00-319-4329AN J79
AEM 8145-00-785-4812AN J79
AEN 8145-00-785-4813AN J79
AEP 8145-00-785-4814AN J79
AER 8145-00-661-2972AS T56
AES 8145-00-887-1949AS T56
AEU 8145-01-070-5771RV TF33
AEV 8145-01-070-5772RV TF33
AEW 8145-01-057-2235RT J75
AEX 8145-01-057-2236RT J75
AEY 8145-00-097-1441 J57
AFA 8145-00-168-6895 TF41
AFB 8145-00-182-6302 TF41
AFC 8145-00-104-5568PQ TF30
AFD 8145-00-139-6187 TF30
AFE 8145-00-413-0987PQ TF30
AFF 8145-00-927-5373PQ TF30
AFG 8145-00-927-5380 TF30
AFH 8145-00-998-4932 TF30
AFJ 8145-00-998-4935 TF30
AFK 8145-00-832-9706 T76
AFL 8145-01-125-1478AN F107-101
AFM 1680-00-677-5227 M9A
AFN 8145-00-839-8418AS T56A7/A9/A15
AFQ 8145-01-125-1473AN F107-400 Engine
AFR 8145-01-116-9590PT F100-24C (Metal)
AFS 8145-00-394-6562PT F100-24F (Metal)
AFT 8145-00-394-6673PT F100-24B (Metal)
AFU 8145-00-928-4859AN T58-100
AFV 8145-01-059-5689AN T700
AFW 8145-01-206-9889AN F112-WR-100
AFX 8145-01-221-3623PT F100-P100
AFY 8145-01-226-7980PT F100-P100
AFZ 8145-01-230-5085PT F100-P100
7-6 Change 1